IEEE TRANSACTIONS ON CIRCUITS AND SYSTEMS-I: REGULAR PAPERS, VOL. 57, NO. 8, AUGUST 2010 1 Analytical Phase Noise Modeling and Charge Pump Optimization for Fractional-N PLLs Frank Herzel, Sabbir A. Osmany, and J. Christoph Scheytt, Member, IEEE Abstract—We present an analytical frequency-domain phase noise model for fractional-N phase-locked loops (PLL). The model includes the noise of the crystal reference, the reference input buffer, the voltage-controlled oscillator (VCO), the loop filter, charge pump device noise, sigma-delta modulator (SDM) noise including its effect on the in-band phase noise. Thermal device noise of the charge pump and the turn-on time of the charge pump output current are found to be limiting the inband phase noise of state-of-the-art synthesizers. Device noise considerations for bipolar transistors and MOSFETs suggest the use of CMOS-only charge pumps (CP), even in BiCMOS technologies. We present a noise-optimized CMOS CP, specifically designed for a dual-loop PLL architecture using two CPs. This PLL architecture keeps the DC output voltage of the noiserelevant CP and the phase noise spectrum constant, regardless of temperature variations. Index Terms—charge pump, fractional-N PLL, phase noise. I. I NTRODUCTION P HASE noise limits the performance of wireless and highspeed digital systems. Frequency synthesizers are commonly characterized in the frequency domain by phase noise spectra. Jitter is the corresponding time-domain equivalent and is used for characterizing clock generation circuits as well as clock and data recovery (CDR) circuits. Several theoretical publications on phase noise and jitter modeling of PLLs have appeared during the last decade, e.g. [1]-[4]. An accurate prediction of phase noise requires simulation on transistor level. However, a complete transistor-level simulation of a PLL is difficult or impossible, even in the absence of noise sources. This is due to very different time scales of the VCO dynamics and the PLL settling. In order to simulate the PLL including nonlinear effects, behavioral system-level simulations are helpful [5]-[11]. An even more simplified approach is linear analytical phase noise modeling, where the main noise contributions are described by adjustable parameters. These models correctly reflect the dependence of the phase noise spectrum on design parameters like loop filter values, charge pump current, divider ratios, etc., but they inevitably need some fit parameters. These can be determined from theory, simulation or measurements. In this paper, we consider only charge-pump PLLs due to their popularity in state-of-the-art synthesizer design. For the Manuscript received October 20, 2009; revised December 8, 2009, accepted December 22, 2009. The authors are with IHP, Im Technologiepark 25, D-15236 Frankfurt (Oder), Germany (e-mail: herzel@ihp-microelectronics.com). Copyright (c) 2009 IEEE. Personal use of this material is permitted. However, permission to use this material for any other purposes must be obtained from the IEEE by sending an email to pubs-permissions@ieee.org. same reason, we assume that the fractional-N divider ratio is obtained by using a sigma-delta modulator (SDM). The SDM in a fractional-N synthesizer inevitably results in large momentary phase errors, even in the absence of noise. This makes the description difficult within an analytical model. Our approach is based on the linear model presented in [12], where the quantization noise spectrum for a multi-stage noise shaping (MASH) SDM was included based on the expression given in [13]. Another critical problem related to SDM noise, which has been disregarded in [12], is the turn-on time of the charge pump (CP), resulting in nonlinearities in the phase detector (PD) as described in [14]-[20]. The combination of an SDM with a nonlinear PD may fold the SDM noise from large frequency offsets down to the in-band region of the spectrum. This effect has been modeled analytically in [18]-[20]. It can be interpreted as self-mixing of the SDM noise in the nonlinear PD, which is composed of phase-frequency detector (PFD) and CP. To avoid confusion with CP device noise and linear SDM noise, this noise contribution will be referred to as PD noise. This paper presents an analytical phase noise model for a PLL including PD noise. The modeled phase noise spectrum and its components are visualized by MATLAB. Finally, a simple CP architecture is suggested, which allows CP device noise and PD noise to be reduced drastically. II. PLL P HASE N OISE S OURCES In a charge-pump PLL as used in modern communication systems, the output phase of the VCO is divided by N and compared with a reference phase in a PFD. A charge pump current proportional to the phase error is produced, low-pass filtered, and applied to the control input of the VCO as shown in Fig. 1. In fractional-N PLLs the divider ratio is controlled by an SDM. REF PFD CP LPF VCO Multi-Modulus Frequency Divider Ctrl Fig. 1. Sigma-Delta Modulator Schematic view of a fractional-N synthesizer architecture. The output voltage of a PLL can be described as Vout (t) = V0 cos[ω0 t + φout (t)] , (1) IEEE TRANSACTIONS ON CIRCUITS AND SYSTEMS-I: REGULAR PAPERS, VOL. 57, NO. 8, AUGUST 2010 where V0 is the amplitude, f0 = ω0 /(2π) is the oscillation frequency, and φout (t) is the excess phase. In this paper, the term phase noise spectrum refers to the two-sided power spectral density (PSD) of φout in units of rad2 /Hz or dBrad2 /Hz, when expressed in decibel. In the latter case, the phase noise is almost identical to the single-sideband phase noise £ in units of dBc/Hz, if and only if white noise sources dominate the PLL noise [4]. The presence of flicker noise results in the well-known 1/f 3 shape of the close-in VCO phase noise spectrum, whereas the single-sideband phase noise spectrum is a Voigt function, which resembles a Gauss function at very small offsets [21]. In this paper, we will include the following seven noise sources: • • • • • • • reference noise, reference input buffer noise, VCO noise, loop filter noise, charge pump device noise, Σ − ∆ quantization noise, phase detector noise. Fig. 2 shows the linearized model of a PLL as presented in [12]. Of special interest in this paper is the PD composed of PFD and CP, which converts a phase error φ at the input into an output current I averaged over one comparison period. For an ideal PD, the gain KPD = dI/dφ is given by ICP /2π, where ICP is the CP current in the ON state. The loop filter transimpedance is denoted as F (s), and the VCO gain is KVCO /s. N is the divider ratio of the PLL. Note that the VCO ICP / 2π π F(s) ICP F (s)KVCO . (2) 2πs For the third-order filter according to Fig. 3, we obtain the H0 = R5 R3 R1 R4 Z1 Z2 C1 Third-order loop filter. KVCO / s F (s) = where Z1 = and 1/Z2 1 , sC3 1/Z1 + 1/Z2 1 R1 + sC1 1/N Linearized PLL model. gain KVCO = dω/dVctrl refers to the angular frequency and || 1 || R4 || R5 sC2 (3) (4) 1 . (5) sC3 Unlike in [12], we have incorporated a voltage divider at the filter input here, which is useful in the context of a dual-loop PLL as discussed in [23]. For a traditional single-loop PLL, R4 and R5 should be omitted or huge values should be used in the noise model. In the following section, the noise sources mentioned in Section II will be analytically described. Z2 = R3 + IV. P HASE NOISE POWER SPECTRAL DENSITY The noise sources discussed in this section are uncorrelated. Therefore, the phase noise PSD at the PLL output is the superposition of the seven mentioned noise contributions, each multiplied by its specific noise transfer function. Emphasis is placed on those components, which are not or only insufficiently included in [12], namely, input buffer noise, charge pump noise and phase detector noise. A. Reference Noise The phase noise contribution of the reference oscillator as a function of the frequency offset f is modeled by SREF (f ) = SREF (∆f ) Fig. 2. C3 C2 transimpedance III. L INEARIZED PLL M ODEL + is given in units of rad/s/V. The forward path transfer function H0 is given by Fig. 3. The latter contribution represents the noise folding of the SDM quantization noise in the nonlinear phase detector. Noise in the frequency dividers is disregarded in this paper, which is focused on phase detector design. It could be added to the phase noise model, if measured phase noise spectra at the feedback divider output and the reference divider output are available. As an alternative, the white spectrum of the inputreferred divider noise can be modeled as a function of delay mismatch in the feedback divider [15], [19]. Another type of noise is caused by digital circuits such as frequency dividers, SDM and PFD, affecting the performance of noise-sensitive analog circuits through supply and substrate coupling. Supplyand substrate-induced jitter may easily exceed device-noiseinduced jitter in high-speed digital systems [22]. φin 2 (∆f )2 + SREF,floor , f2 (6) where SREF (∆f ) is the phase noise at a specific offset ∆f in the -20dB/decade region of the spectrum and SREF,floor is the noise floor of the reference. The reference noise spectrum at the output reads out SREF = SREF N 2 |H|2 (7) IEEE TRANSACTIONS ON CIRCUITS AND SYSTEMS-I: REGULAR PAPERS, VOL. 57, NO. 8, AUGUST 2010 with the transfer function given by H= H0 /N . 1 + H0 /N (8) B. Reference Input Buffer Noise As discussed in [23], the noise of the reference buffer may become a major contributor to the output phase noise. We use an ESD protected CMOS inverter chain as input buffer shown in Fig. 4. The first CMOS inverter converts the 3 where kB is Boltzmann’s constant, T is the absolute temperature, and YFIL = 1/Z1 + 1/Z2 is the complex admittance of the filter from the charge pump output to ground. The resulting noise spectrum at the output is given by 2 2 KV CO 2 out SFIL (s) = SFIL (s) |F (s)| |1 − H| . (13) s E. Charge Pump Device Noise For a PLL to work at a given bandwidth, a large charge pump current is generally favorable in order to reduce the loop filter resistance R1 . The large current, however, produces significant current noise. The time between two phase comparison instants is referred to as Ts = 1/fs , where fs is the frequency at the PFD input at which the PLL phase error is sampled. In order to describe the thermal CP noise qualitatively, we write the two-sided thermal drain current noise PSD of a MOSFET according to [24] as SiMOS = γ 2kB T gDS0 , Fig. 4. Proposed input buffer (a) and noise model (b). crystal oscillator signal into a rectangular signal on the chip. Assuming a sinusoidal reference signal with peak amplitude V0 , we obtain for the phase noise at the PLL output out = SBUF SVBUF 2 N |H|2 , V02 (9) where SVBUF is the input-referred noise voltage PSD. The transconductance of the MOSFETs (∝ W/L) must be large enough to make this noise negligible. C. VCO Noise The phase noise of a free running oscillator is modeled by (∆f )2 fcVCO SVCO (f ) = SVCO (∆f ) + Sfloor , (10) 1 + f2 f where SVCO (∆f ) is the phase noise at a specific offset ∆f in the -20dB/decade region of the spectrum, fcVCO is the 1/f 3 noise corner of the VCO, and Sfloor is the noise floor of the VCO. The PLL output noise due to VCO phase noise is given by out SVCO = SVCO |1 − H|2 , (11) where H is given by (8). where gDS0 is the channel conductance with zero drain-source voltage, and γ is between 2/3 and 1 for long-channel devices and somewhat larger for short devices, typically 1-3. This type white of the charge of noise results in a white noise spectrum SCP pump described by one parameter. This parameter can be fitted to measurements or simulated by periodic steady-state analysis (PSSA) [8]. Thermal noise must be multiplied by the CP duty cycle αCP = TON /Ts , where TON is the CP activation time. In addition to thermal noise, CPs also exhibit flicker noise 2 (1/f noise). The flicker noise PSD is proportional to αCP [25]. This is due to the large auto-correlation time of this type of noise, which is assumed to be much larger than Ts . Adding the two noise contributions, we obtain αCP fc white , (15) SCP = SCP αCP 1 + f where fc is the 1/f noise corner frequency of the transistor. Note that the flicker noise corner of the CP scales with αCP , which usually makes flicker noise small compared to thermal noise, unless a large CP duty cycle is used. For the white noise white current PSD normalized to the CP current SCP /ICP we −19 found a value of 6×10 A/Hz for the cascode CP from [23]. This value was obtained by a PSSA followed by a periodic noise analysis using Virtuoso Analog Design Environment. More details will be given in Section VI. The noise spectrum at the PLL output reads 2 2 2 KVCO out |1 − H| . (16) SCP = SCP |F (s)| s F. Sigma-Delta Quantization Noise D. Loop Filter Noise We model the noisy loop filter by a noise current in parallel with a noise-less admittance. The two-sided power spectral density of noise current in can be expressed as SFIL (s) = 2kB T Re(YFIL (s)) , (14) (12) The quantization noise spectrum for an m-th order MASH type SDM is given by [13] 2(m−1) (2π)2 πf SSDM = 2 sin , (17) 12fs fs IEEE TRANSACTIONS ON CIRCUITS AND SYSTEMS-I: REGULAR PAPERS, VOL. 57, NO. 8, AUGUST 2010 where m is the order of the modulator. The SDM noise spectrum at the PLL output is given by out SSDM = SSDM |H|2 . (18) G. Phase Detector Noise If both UP and DOWN current are changing in the steady state of the PLL, then the phase detector gain will be discontinuous, if UP and DOWN currents do not match. This case has been discussed in [20]. For a low-noise PLL in fractional-N mode, an offset current at the CP output is highly recommended as shown in [16]. If the offset current is a sufficiently large down current, then only the UP current will respond to phase error changes in the steady state. This improves the linearity of the phase detector and reduces phase noise significantly. In this case, the output current I of the CP is a continuous function of the phase error φ at the PFD input, ideally a linear function. In reality, the limited turn-on time of the current will result in deviations from this behaviour. Taking the nonlinearities into account in the lowest order, we can write the current as β (19) I = φ KPD (1 + φ) , 2 where KPD is the linear PD gain, and β represents the firstorder nonlinearity. It can be determined from dI/dφ = KPD (1 + β φ) , (20) resulting in β = (d2 I/d φ2 ) /KPD . The linear term in (19) produces the quantization noise spectrum described in Section IV-F, and the quadratic term will cause the PD noise discussed in this sub-section. Third-order nonlinearities in the PD transfer function have been disregarded in this paper. Such nonlinearities have been modeled in [10] in the zero phase offset region. Fig. 5 shows the simulated PD gain dI/dφ as a function of the phase error at the PFD input for the cascode CP used in [23]. Here, the sampling frequency fs was Gain [mA/rad] −∞ with ω = 2πf and the brackets < ... > denoting the stochastic (ensemble) average. Substituting (19) into (21) we obtain 2 2 SI (f ) = KPD < I1 > +KPD β < I2 > + 2 β2 KPD < I3 > 4 (22) with the integrals I1 (f ) = Z ∞ φ(t + τ ) φ(t) exp(−jωτ ) dτ, (23) φ(t + τ ) φ2 (t) exp(−jωτ ) dτ, (24) −∞ I2 (f ) = Z ∞ −∞ and I3 (f ) = Z ∞ φ2 (t + τ ) φ2 (t) exp(−jωτ ) d τ. (25) −∞ The first term in (22) corresponds to the term SSDM discussed in Section IV-F. The other terms describe noise folding contributions. If the process φ(t) is symmetric with respect to the sign, positive and negative contributions in I2 will cancel out. In order to calculate I3 , we decompose φ(t) into a Fourier integral Z ∞ φ(f ) exp(jωt) df. φ(t) = (26) −∞ Equation (25) then reads Z Z Z Z Z I3 (f ) = φ(f1 ) φ(f2 ) φ(f3 ) φ(f4 ) exp[jω4 t] exp(−jωτ ) dτ df1 df2 df3 df4 , Slope: 0.035 mA / rad −1.20 2 −1.25 linear fit δ(f1 + f2 − f ) exp[jω1 t] exp[jω2 t] simulated −1.30 exp[jω3 t] exp[jω4 t] df1 df2 df3 df4 . −2 −1 0 1 (27) where all integrals are to be taken from −∞ to +∞. Integration with respect to τ yields Z Z Z Z I3 (f ) = φ(f1 ) φ(f2 ) φ(f3 ) φ(f4 ) β=0.028 / rad 2 Phase Error [rad] Fig. 5. offsets in the nonlinear PD. Note that the PD gain is a fairly linear function of the input phase error over a wide range. In other words, the parabolic approximation of the PD transfer function given by (19) seems reasonable for this particular CP. In order to calculate the two-sided spectrum of the CP current, we write it as the Fourier transform of the auto-correlation function (ACF) according to the Wiener-Khintchine theorem Z ∞ hI(t + τ ) I(t)i exp(−jωτ ) d τ (21) SI (f ) = exp[jω1 (t + τ )] exp[jω2 (t + τ )] exp[jω3 t] −1.15 −1.35 4 Phase detector gain versus input phase error for cascode CP. 100 MHz, and the CP current was as large as 8 mA for a low in-band phase noise. As evident from Fig. 5, the PD gain is not constant but depends on the phase error, which causes noise folding in the PLL. More specifically, the quantization noise described in Section IV-F is folded down to low frequency Integration with respect to f2 , f3 and f4 results in Z ∞ φ(f1 ) φ(f − f1 ) φ2 (t) df1 . I3 (f ) = (28) (29) −∞ Taking the average on both sides yields Z ∞ 2 < φ(f1 ) φ(f − f1 ) > df1 . < I3 (f ) >= σφ (30) −∞ The PD noise is basically a convolution of the SDM phase noise with itself, multiplied by the variance of the phase. In IEEE TRANSACTIONS ON CIRCUITS AND SYSTEMS-I: REGULAR PAPERS, VOL. 57, NO. 8, AUGUST 2010 the context of close-in phase noise, the low-frequency limit is relevant. We obtain for f = 0 Z ∞ < |φ(f1 )|2 > df1 , (31) < I3 (0) >= σφ2 −∞ where we have exploited the property φ(−f ) = φ∗ (f ) for the real-valued process φ(t). For the PD noise we obtain 2 2 KPD β2 2 KVCO 2 out < I3 (f ) > |F (s)| SPD (f ) = |1 − H| 4 s (32) where the same transfer function as for the CP noise current was used. For Gaussian noise of φ, we can further simplify the result for the in-band phase noise due to the nonlinear PD. The net charge delivered by the charge pump and the resulting squared phase error φ2 are sampled at the rate fs = 1/Ts . From the Nyquist-Shannon sampling theorem we know that this sampled process can be expressed by a continuous-time signal the spectrum of which has no Fourier components above the Nyquist frequency fs /2. We assume similarly to [18] and [20] that the spectrum Sφ2 (f ) of φ2 is white for −fs /2 < f < fs /2. The variance of φ2 then follows by integration of Sφ2 (f ) and reads (33) The quadratic term in (19) results in the PD noise current spectrum 2 2 β Sφ2 . (34) SPD = KPD 4 Substituting (33) into (34) and multiplying the result by the noise transfer function, we obtain out (f ) SPD = 2 KPD β2 < φ4 > − < φ2 >2 × 4 fs 2 2 KVCO 2 |F (s)| |1 − H| . s phase noise is proportional to σφ4 , that is, a reduction of σφ by a factor of two will lower the phase noise by 12 dB. Therefore, for a relatively poor PD linearity as in [23] a single-loop SDM might be the better choice, since the momentary phase error and σφ are lower than for a MASH type SDM [14]. A reduction of the nonlinearity parameter β by a factor of 10 will reduce the in-band PD noise by 20 dB as evident from (38). Therefore, a MASH type SDM might be the better choice for a highly linear PD as proposed in Section VI. It has the advantage of easy integration in CMOS or BiCMOS and is unconditionally stable. V. PLL P HASE N OISE S PECTRUM Since the noise sources are uncorrelated, the corresponding noise spectra must be added to obtain the total phase noise spectrum at the PLL output given by out out out S out (f ) = SREF (f ) + SBUF (f ) + SVCO (f ) + out out out out SFIL (f ) + SCP (f ) + SSDM (f ) + SPD (f ) , (39) out out out out out where SREF (f ), SBUF (f ), SVCO (f ), SLPF (f ), SCP (f ), out out SSDM (f ), and SPD (f ) are the phase noise contributions of the previously discussed noise sources referred to the PLL output. The rms phase error [degree] at the PLL output, sometimes called absolute phase jitter, is given by sZ ∞ ◦ 180 2 S out (f ) df . (40) σφout = π 0 Fig. 6 shows the simulated phase noise spectrum and the components for a 10 GHz frequency synthesizer, which employs a cascode charge pump. Here, the model parameters -60 σφ=1.43o -70 (35) For a high order of the SDM, the probability density of φ is approximately Gaussian. By using partial integration, we obtain the averages in (35) given by Z ∞ 2 φ2 exp (−φ2 /2σφ2 ) dφ = σφ2 (36) < φ2 >= √ 2πσφ 0 CP Phase Noise [dBc/Hz] σφ2 2 =< φ4 > − < φ2 >2 = Sφ2 fs . 5 -80 Total REF PD -90 VCO BUF -100 -110 SDM LPF -120 and < φ4 >= √ 2 2πσφ Z 0 -130 ∞ φ4 exp (−φ2 /2σφ2 ) dφ = 3σφ4 . (37) By substituting (36) and (37) into (35) we finally obtain 2 2 KPD β 2 σφ4 2 2 KVCO out |1 − H| . (38) SPD (f ) = |F (s)| 2 fs s Note that we have a close similarity to the analytical result of Mao [20], where β 2 /2 corresponds to the mismatch parameter γ in [20] and σφ2 corresponds to σ(|∆φ|). The same result could not be expected, since [20] considers the case of a discontinuous PD gain due to mismatch between UP and DOWN current, whereas we consider the case of a continuous PD gain realized by an offset current at the CP output. The -140 102 103 104 105 106 107 108 Frequency Offset [Hz] Fig. 6. Modeled phase noise spectrum for a 10 GHz synthesizer using a cascode charge pump. have been adapted to measurements on the experimental dualloop PLL presented in [23]. For space limitations, we only sketch this process here. First, the noise of the 100 MHz crystal oscillator mounted on the PCB was measured by a spectrum analyzer. Subsequently, the noise of the input buffer was measured using small sinusoidal input signals to maximize the reference buffer noise. The VCO noise spectrum IEEE TRANSACTIONS ON CIRCUITS AND SYSTEMS-I: REGULAR PAPERS, VOL. 57, NO. 8, AUGUST 2010 was determined from phase noise measurements on the freerunning oscillator. For the noise contributions of the loop filter and the SDM no parameters but the filter values and the SDM order are required. In order to model the PD noise, the rms phase error σφ was estimated from MATLAB simulations and the curvature parameter β was obtained from transient circuit simulations using the simulator Virtuoso Analog Design Environment. Charge pump device noise was also modeled by circuit simulation. Details of these simulations will be given in Section VI-C. Unlike in traditional PLLs, the VCO phase noise is bandstop filtered due to the presence of the voltage divider R4/R5 at the charge pump output as shown in Fig. 3. For the same reason, all other noise transfer functions are modified at low frequencies. These modifications are not critical, provided that the biasing resistors are not too small. The relatively high level of PD noise can be explained by the high PLL output frequency of 10 GHz in conjunction with strong PD nonlinearity and the employment of a MASH type SDM, which results in a large rms phase error in fractional-N mode. In our example, the PD noise due to CP nonlinearity and the CP device noise dominate the in-band phase noise. This was the main motivation for improving the CP with respect to linearity and device noise as discussed in the following section. VI. S UGGESTED N OVEL C HARGE P UMP In this section, we will consider the output noise PSD of a bipolar transistor and a MOSFET. The potential of MOSFETs with large gate-source voltages in the context of low-noise CPs is outlined. This is followed by a brief description of a low-noise dual-loop PLL architecture with CP output biasing. Subsequently, we describe a simple CP architecture specifically designed for VCO fine tuning using this PLL architecture. An improvement by 10 dB over the existing design from [23] with respect to CP thermal device noise and PD noise is predicted. A. Transistor Noise Considerations This paper was motivated by the desire to improve the synthesizer for space applications in SiGe-BiCMOS technology. BiCMOS technologies offer the opportunity to choose between bipolar transistors and MOSFETs for the best design of each building block. Generally, bipolar transistors have the reputation to provide better high-frequency noise performance than MOSFETs, which is only partly true. This reputation mainly results from the large transconductance of (hetero-) bipolar transistors compared to MOSFETs. While this advantage is crucial for amplifiers, this is not necessarily the case for other circuits like charge pumps. Here, the white device noise in the output circuit (drain or collector) must be compared for the two devices. A transformation to the gate or base terminal as typically performed in low-noise amplifiers is not meaningful here. In the following, we compare the white output noise power spectral densities (PSD) for the two types of devices. The two-sided thermal drain current noise PSD of a MOSFET was according to (14) SiMOS = γ 2kB T gDS0 . (41) 6 In saturation, the transconductance gm is given by sat gm = 2ID /Vov = gDS0 , (42) where the gate-source overdrive voltage Vov = VGS − Vth was introduced. By substituting (42) in (41) we obtain SiMOS = 4γkB T ID . Vov (43) The two-sided shot noise PSD of a bipolar transistor is given by SiBip = qIC , (44) where IC is the DC collector current and q is the elementary charge. Assuming the same DC current for the two transistors, we obtain from (43) and (44) for the ratio between the output current noise PSDs 208 mV 4γVT ≈ . (45) SiMOS /SiBip = Vov Vov Here we assumed γ ≈ 2 and T = 300 K, resulting in a thermal voltage VT = kB T /q of 26 mV. We conclude that MOSFETs may show much less white output noise compared to their bipolar counterparts, provided that the overdrive voltage is much larger than 200 mV. Obviously, the advantage of MOSFETs over bipolar transistors is especially pronounced for processes with a higher CMOS supply voltage. This advantage reduces with technology scaling, which makes MOSFETs less attractive for low-voltage applications. We have disregarded flicker noise in this comparison. We believe that flicker noise is less important than thermal noise for the following reason. The CP flicker noise corner is given by αCP fc according to (15). Assuming a transistor noise corner of 1 MHz and a duty cycle of 10 percent, we obtain a CP flicker noise corner of 100 kHz. The optimum loop bandwidth is typically larger in a fractional-N PLL, suppressing flicker noise in the CP efficiently. We will show that the condition Vov >> 200 mV can be fulfilled by employing the modern dual-loop PLL architecture from Section VI-B in conjunction with the CP architecture from Section VI-C. This architecture will allow the gate-sources voltages to be fully switched between ground (VSS) and CMOS supply (VDD=2.5 V in our case). For the CP MOSFETs might be the better choice compared to SiGe-HBTs, whereas HBTs are better suited for low-noise VCOs and frequency dividers at high frequencies due to the large transconductance compared to MOSFETs. Moreover, the flicker noise performance of SiGe-HBTs based VCOs is much better [26]. B. PLL Architecture for Low Phase Noise A dual-loop architecture using two parallel CPs was described in [23] and [27]. A slightly modified version is suggested in Fig. 7. Here, the two charge pumps CP1 and CP2 for fine and coarse tuning, respectively, are composed of five binary weighted CPs each, selectable by a common five-bit control line. Two current sources (CS) are added to generate offset currents IOS1 and IOS2 in the fine tuning loop and the coarse tuning loop, respectively. They are composed of five binary weighted CSs each, which are controlled by another IEEE TRANSACTIONS ON CIRCUITS AND SYSTEMS-I: REGULAR PAPERS, VOL. 57, NO. 8, AUGUST 2010 CS_ctrl<4:0> CS1 0-2 mA OUT CP_ctrl<4:0> FINE COARSE VCO DIV CP1 0-8 mA LPF PFD CP2 0-600 µA BAND SELECT REF Digital Control CS2 0-150 µA 7 with moderate gate-source voltages VGS or moderately sized MOSFETs with large VGS can be used. From (43) we conclude that the latter option results in a lower device noise. The next step in the design of a low-noise CP is to find an architecture, where the gate-source voltages are maximized. The simplest CP with this property consists of a pMOSFET M1 delivering the UP current and an nMOSFET M2 delivering the down-current. Such a circuit is shown in Fig. 8. Unlike conventional CPs, it does not use cascode transistors or current mirrors, which avoids additional potential noise sources. A Vdd Fig. 7. Schematic view of dual-loop frequency synthesizer. five-bit control line. The advantage of an offset current at the CP output is the opportunity to shift the steady-state operation point of the phase detector in order to improve its linearity [28], [16]. Since the two CPs are driven by the same PFD, the condition IOS1 /ICP1 ≈ IOS2 /ICP2 should be fulfilled in order to keep the DC value of the fine tuning voltage constant. The noise in the low-current charge pump CP2 for coarse tuning is minimized by a large capacitor to ground (100 nF in [23]). As a result, the phase noise is dominated by the fast fine tuning loop. Due to the low fine-tuning gain of the VCO the overall phase noise is significantly reduced compared to a single-loop PLL with the same tuning range as experimentally verified in [23]. This improvement is especially important for fractionalN PLLs, where the large CP duty cycle increases phase noise and spurs, particularly, if a DC offset current is added to the CP output current. C. Charge Pump Architecture for Low Phase Noise In most cases, charge pumps have been designed and optimized for single-loop PLLs. A vast number of publications is devoted to this topic, see [29], [30] and references therein. In order to obtain a good matching between UP and DOWN currents over the whole PLL tuning range, a large output resistance of the CP is generally mandatory for single-loop PLLs. The situation is completely different, if a CP is used for fine tuning of the VCO only, where its output DC voltage is almost fixed as in [23]. In this case, emphasis can be placed on fast current switching of the CP and on a low device noise by simplifying the CP architecture. In this paper, we confine ourselves to this dual-loop PLL architecture and consider only the charge pump for fine tuning. For coarse tuning, a traditional low-current CP with a higher output impedance could be used. As was shown in Section VI-A, MOSFET-based CPs can provide a low white noise, if their gate-source voltages are large. In addition, they also exhibit flicker noise. However, the flicker noise corner frequency of the CP given by αCP fc according to (15) is lower than the transistor noise corner by the factor αCP . Since αCP is typically lower than 10 percent, flicker noise is usually less important than thermal noise in the context of CP design. The CP current ICP is usually determined from system simulations and results in a given drain current ID of the CP output transistors. In order to generate the drain current ID , either large MOSFETs UP R5 M1 OUT DOWN M2 CS M3 R4 Vss Fig. 8. Charge pump architecture used in CP1. switchable CS realized by the transistor M3 between the output and ground was also introduced to improve the PD linearity. At first sight, this CP seems unacceptable for low-noise PLL design, since the output resistance is rather low, and the matching between UP and DOWN current extremely depends on the output voltage. In traditional single-loop PLLs this would inevitably result in large spurs and a strong dependence of the PLL phase noise spectrum on the output frequency. However, these problems are solved, if this CP is used for fine tuning of the VCO (CP1 in Fig. 7), whereas a traditional lowcurrent CP is used for coarse tuning (CP2 in Fig. 7). The noise of the latter can be reduced to a negligible level by loading it with a large capacitor [23]. A voltage divider composed of two resistors R4 and R5 on the order of 1 kΩ is added at the output of CP1 to stabilize the DC output voltage at a desired value given by VDD×R4/(R4+R5). This eliminates the need for a high output impedance of CP1 and improves its performance. At the same time, the VCO fine tuning gain is kept almost constant, which makes the PLL phase noise spectrum robust with respect to device parameter variations with process, supply voltage and temperature (PVT variations). Note that the PVT dependence of the CP itself is larger than for a typical cascode CP. However, the loop bandwidth in a CP PLL is proportional to the product KVCO ICP . In an integrated VCO, the gain can easily vary by a factor of three or more over the tuning range. By contrast, variations in the threshold voltage of magnitude ∆V cause relative changes of the charge pump current on the order of 2∆V /Vov ≈ 2∆V /V DD only, as evident from (42). This is much smaller than relative KVCO changes in a single-loop PLL. The relatively constant loop bandwidth over a wide tuning range in a dual-loop PLL using a cascode CP with output biasing has been experimentally demonstrated in [27] and [23]. The low output impedance of our new CP will reduce supply rejection. However, will believe this drawback to be less significant than the advantage IEEE TRANSACTIONS ON CIRCUITS AND SYSTEMS-I: REGULAR PAPERS, VOL. 57, NO. 8, AUGUST 2010 Charge Pump Currents [mA] 8 IUP 6 IDOWN 4 IOFFSET 2 0 79 80 −1.25 2 Slope: −0.0019 mA / rad Gain [mA/rad] of having a highly linear CP with a low thermal device noise. To minimize the effect of CP supply noise on the VCO, an on-chip voltage regulator and a separate CP supply would be helpful. The CP draws an additional DC current VDD/(R4+R5) due to output biasing. This results in a trade-off between power consumption and phase noise. The fractional-N PLL in [23] uses R4=R5=1 kΩ to stabilize the output DC voltage of the CP generating a current up to 8 mA. This choice was motivated by the desire to minimize the phase noise, whereas power consumption was considered less critical in satellite applications. By contrast, the integer-N PLL for 60 GHz wireless communications in [27] used R4=R5=100 kΩ. Generally, R4 and R5 should be larger for integer-N PLLs compared to fractional-N PLLs due to the lower CP duty cycle of the former. Moreover, CMOS VCOs require larger resistors R4 and R5 than bipolar oscillators to guarantee sufficient flicker noise suppression in the loop. Fig. 9 shows the simulated charge pump currents in the fine tuning loop for two different offset currents. Obviously, 8 β=−0.0015/rad −1.26 linear fit simulated −1.27 −1.28 −2 −1 0 1 2 Phase Error [rad] Fig. 10. Phase detector gain versus input phase error for new charge pump. the PFD input for the new CP. It was calculated by simulating the average CP output current as a function of the input phase error and numerically differentiating the result with respect to the phase error. The PD gain dI/dφ = ICP /2π=8 mA/2π ≈ 1.27 mA/rad is almost the same as in Fig. 5 to make the two CPs comparable. The slope of this gain curve is essentially the curvature of the phase detector characteristic I(φ) according to (20) and below. The average slope is lower by a factor of 18 compared to the cascode CP gain in Fig. 5. This improvement of the linearity is expected to have a significant effect on the in-band phase noise and spurs of the fractional-N PLL. In addition to improving the PD linearity, the new CP reduces thermal device noise. Fig. 11 shows the simulated device noise of the new CP and of the cascode CP used in [23]. Note that the large duty cycle of 30 percent represents 81 Time [ns] Fig. 9. Simulated UP and DOWN currents of CP1 and offset current IOS1 for two offset current levels. the short DOWN current pulse is not affected by the offset current, whereas the UP current pulse becomes broader with increasing offset current. This allows the phase detector to be linearized by shifting the operation point into a region, where only the UP current responds to the inevitable phase error changes in fractional-N mode [16]. In order to obtain a high linearity of the PD, the current pulses should be as steep as possible. This is achieved in our CP architecture by the large swings and the steep waveforms of the gate-source voltages toggling between VSS and VDD. As a result, the turnon time and turn-off time are as low as 250 ps and 200 ps, respectively, which is approximately one inverter delay. The turn-on time is about four times shorter than the value of 1 ns reported for a charge pump in 0.35 µm CMOS technology using a cascode architecture [31]. Cascode architectures can provide a high output resistance and good current matching, but the swing of the gate-source voltages of the switching MOSFETs is significantly smaller than VDD, limiting their turn-on times and, thereby, the PD linearity. Fig. 10 shows the simulated PD gain dI/dφ as a function of the phase error at ICP = 4mA αCP = 30% Cascode CP New CP Fig. 11. Simulated output noise current PSD for new CP (lower curve) and cascode CP. a worst case with respect to CP device noise. For a 100 MHz reference as in [23], this duty cycle corresponds to a CP activation time TON of 3 ns, which is sufficiently large to linearize the PD, even if a MASH SDM with its large rms phase error is employed. The noise plateau is reduced by 10 dB IEEE TRANSACTIONS ON CIRCUITS AND SYSTEMS-I: REGULAR PAPERS, VOL. 57, NO. 8, AUGUST 2010 as a result of the larger gate-source voltages and the small number of transistors. Remember that the noise corner of the CP is proportional to αCP according to (15). This long-term correlation effect is not correctly reflected by the simulation, which overestimates the 1/f noise by a factor of 1/αCP . For typical values of αCP =1-10 percent, this corresponds to 1020 dB. However, the white noise plateau is correctly modeled. Therefore, we can expect a reduction of the in-band noise contribution in the phase noise plateau by 10 dB for the new CP. As assumed in (15), the noise current PSD SCP due to thermal device noise is expected to be proportional to the CP duty cycle. In order to confirm this assumption and to white determine the ratio SCP = SCP /αCP , we have simulated the high-frequency noise PSD over a wide range of αCP . Fig. 12 shows the simulated device noise for different phase errors corresponding to different CP duty cycles. For the white 2 Current PSD [(pA) /Hz] 200 linear fit 150 100 50 0 2 Slope: 250 (pA) /Hz 0 20 40 60 9 PLL output by using σφout 1800 = π sZ fmax df 2 Sout (f) , (46) fmin where we employ fmin = 100 Hz and fmax = 100 MHz as integration limits. In high-speed digital design, the absolute PLL jitter (or tracking jitter) is often used for noise characterization. It describes the deviation of the zero crossings of the output clock from the ideal positions, where a clean input clock is assumed. Absolute PLL jitter is given by σφout T0 , (47) 3600 where T0 = 1/f0 is the ideal period of the PLL output signal. In CDR circuits, the output signal is often referred to itself shifted by a delay τ . For a very long delay τ , the autocorrelation of the output signal converges to zero, and the self-referenced jitter σSR (τ ) approaches a steady-state value σSR (∞). If white noise sources dominate the√phase noise, then we find for the long-term jitter σSR (∞) = 2 σabs as shown in [32]. In conclusion, the improvement of the charge pump will not only reduce the phase noise, but also rms phase error, absolute jitter and long-term jitter. In order to predict the expected improvement, we assume a reduction of white charge pump device noise by 10 dB and a reduction of β by a factor of 10. These numbers are consistent with the simulations presented in Section VI. Fig. 13 shows the simulated phase noise spectrum and its components for this case. The PD noise σabs = αCP [percent] -60 Fig. 12. Simulated output current PSD at 10 MHz as a function of CP duty cycle αCP for ICP =4 mA. VII. I NTEGRATED P HASE E RROR AND T IMING J ITTER Timing jitter and phase noise describe the same physical effect. Timing jitter describes the fluctuations of the zero crossings of the output signal around the ideal values, whereas phase noise is the corresponding frequency-domain equivalent. In RF synthesizer design, the rms phase error is often used as a metric to quantify the overall phase noise performance. We calculate the integrated rms phase error σφout [degree] at the Phase Noise [dBc/Hz] white noise current PSD normalized to the CP current SCP /ICP −20 we found a value of 6.3 × 10 A/Hz for this CP, which is an order of magnitude lower than for the cascode CP. As an illustration, we consider a 10 GHz PLL driven by a 100 MHz reference using a 4 mA CP in the fine tuning loop. Assuming a duty cycle αCP of 20 percent, we obtain in an input-referred white phase noise SCP = SCP /(ICP /2π)2 −16 2 of 1.25 × 10 rad /Hz. This corresponds to a phase noise of -159 dBrad2 /Hz or -159 dBc/Hz, as follows from the remark after (1). At the 10 GHz PLL output this noise appears amplified by 20 log(10 GHz/100 MHz) = 40 dB, resulting in an in-band phase noise due to thermal charge pump noise of -119 dBc/Hz. This noise level is negligible compared to other noise sources as evident from Fig. 6. -70 σφ=0.75o CP -80 REF Total -90 VCO BUF -100 -110 PD SDM -120 LPF -130 -140 102 103 104 105 106 107 108 Frequency Offset [Hz] Fig. 13. Modeled phase noise spectrum for a 10 GHz synthesizer using the novel charge pump for fine tuning. due to CP nonlinearity is now almost negligible, which can be understood from equation (38). Since the PD phase noise is proportional to β 2 , the linearity improvement by a factor of 10 will lower this phase noise contribution by 20 dB. As a result, the integrated phase error is reduced from 1.43 to 0.75 degree. The latter value corresponds to an absolute jitter of σabs = (0.750 /3600 )/10GHz = 0.21 ps for our 10 GHz PLL. This value is much lower than the best reported values for CMOS clock generators [33]. IEEE TRANSACTIONS ON CIRCUITS AND SYSTEMS-I: REGULAR PAPERS, VOL. 57, NO. 8, AUGUST 2010 VIII. C ONCLUSION We have presented analytical expressions for the phase noise spectrum of phase-locked loops. The results were visualized by MATLAB. For an existing design, thermal noise and nonlinearity of the charge pump were found to be critical with respect to phase noise. A method was proposed to reduce these noise contributions drastically. 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Heyer, “An integrated 18 GHz fractional-N PLL in SiGe BiCMOS technology for satellite communications,” in Proc. of 2009 IEEE Radio Frequency Integrated Circuits Symposium (RFIC 2009), Boston, USA, June 2009, pp. 329-332. [24] B. Wang, J. R. Hellums and C. K. Sodini, “MOSFET thermal noise modeling for analog integrated circuits,” IEEE Journal of Solid-State Circuits, vol. 29, pp. 833-835, July 1994. [25] A. Lacaita, S. Levantino and C. Samori, Integrated Frequency Synthesizers for Wireless Systems, New York: Cambridge University Press, 2007. [26] G. Niu, “Noise in SiGe HBT RF technology: physics, modeling, and circuit implications,” Proceedings of the IEEE, vol. 93, pp. 1583-1597, Sep. 2005. “Comprehensive behavioral modeling of conventional and dual-tuning [27] F. Herzel, S. Glisic, S. A. Osmany, J. C. Scheytt, K. Schmalz, W. PLLs,” IEEE Transactions on Circuits and Systems-I: Fundamental Winkler, and M. Engels, “A fully integrated 48-GHz low-noise PLL with Theory and Applications, vol. 55, pp. 1628-1638, July 2008. a constant loop bandwidth,” in Proceedings of the 2008 Topical Meeting [12] S. A. Osmany, F. Herzel, K. Schmalz, and W. Winkler, “Phase noise and jitter modeling for fractional-N PLLs,” Advances in Radio Science, vol. 5, 2007. [13] B. Miller, “A multiple modulator fractional divider,” IEEE Transactions on Instrumentation and Measurements, vol. 40, pp. 578-583, June 1991. on Silicon Monolithic Integrated Circuits in RF Circuits (SiRFIC 2008), Orlando, USA, Jan. 2008, pp. 82-85. [28] Thomas H. Lee, The Design of CMOS Radio-Frequency Integrated Circuits, pp. 459, New York: Cambridge University Press, 1998. [29] W. Rhee, “Design of high-performance CMOS charge pumps in phase- IEEE TRANSACTIONS ON CIRCUITS AND SYSTEMS-I: REGULAR PAPERS, VOL. 57, NO. 8, AUGUST 2010 locked loops,” in Proc. of the 1999 IEEE International Symposium on Circuits and Systems (ISCAS ’99), vol. 2, June 1999, pp. 545-548. [30] J. Rogers, C. Plett, and F. Dai, Integrated Circuit Design for High-Speed Frequency Synthesis, Norwood: Artech House, 2006. [31] K. Shu, E. Sánchez-Sinencio, J. Silva-Martinez, and S. H. K. Embabi, “A 2.4-GHz monolithic fractional-N frequency synthesizer with robust phase-switching prescaler and loop capacitance multiplier,” IEEE Journal of Solid-State Circuits, vol. 38, pp. 866-874, June 2003. [32] J. A. McNeill, “Jitter in ring oscillators,” IEEE Journal of Solid-State Electronics, vol. 32, pp. 870-879, June 1997. [33] F. H. Gebara, J. D. Schaub, A. J. Drake, K. J. Nowka, and R. B. Brown, “4.0GHz 0.18µm CMOS PLL Based on an Interpolative Oscillator,” 2005 Symposium on VLSI Circuits Digest of Technical Papers, Honolulu, USA, June 2005, pp. 100-103. PLACE PHOTO HERE PLACE PHOTO HERE Frank Herzel was born in Güstrow, Germany in 1963. He received his M.S. degree in Berlin (1989) and his Ph.D. in Rostock (1993), both in theoretical physics. Since 1993 he has been with the IHP in Frankfurt (Oder), where he was mainly involved in semiconductor device modeling until 1996. Since then he has been working in the design of silicon IC’s for RF communications. Currently, he is focusing on SiGe BiCMOS frequency synthesizers for space applications. Sabbir A. Osmany was born in Bangladesh in 1975. He received his M.S. degree from University of Ulm, Germany in Communications Technology. Since 2005 he is with the IHP, where he is working towards the Ph.D. degree. His research interest involve mixed-signal and RF IC design for wireless or optical communication with emphasis on integer-N and fractional-N frequency synthesizers. J. Christoph Scheytt (M’01) received his diploma degree (M.S., 1996) and Ph.D. degree (2000, with highest honors) both from Ruhr-University Bochum, Germany. In 2000 he co-founded advICo microPLACE electronics GmbH, a German IC design house. For PHOTO 6 years he served as CEO at advICo where he HERE was responsible for various projects in the area of wireless and fiber-optic IC design. Since 2006 he is with IHP where he is head of circuit design department, a group of about 30 researchers working on high-frequency and broadband IC design. Dr. Scheytt has authored and co-authored more than 40 papers and holds 6 patents. His research interests include RFIC and broadband IC design, PLL techniques, and design with SiGe BiCMOS technologies. 11