Chapter 4 Transconductance-C Filters
4.2 Elementary Transconductor Building Blocks
4.2.1 Resistors
In general, there is little need for resistors in the area of Gm-C filters except source and load resistors in doubly terminated LC ladders. For low-sensitivity design, source and load resistors should be taken into consideration. The transconductor-based resistors are shown in Fig. 4.1.
Fig. 4.1 Resistor Simulates with Transconductors
For Fig. 4.1(a), since the transconductor input is ideally an open circuit, the input current Ii is equal to the transconductance output current Io as
i m o
i I g V
I = = (4.1) As a result, the equivalent resistance is
m i
i
g I
R V 1
=
= (4.2)
In Fig. 4.1(b), we connect the two inputs to two different voltages, and feed the outputs back to the inputs. The relation between input currents and output voltage can be described as
) (V1 V2 g
I I
Ii = o = = m − (4.3)
Consequently, the resistor is
gm
I V
R=V1− 2 = 1 (4.4)
Observing the results found in Fig. 4.1(a) and Fig. 4.1(b), we know that the negative feedback cause the positive resistors. On the other hand, a negative resistor,
m i
i I R g
V =− =−1 , by using the positive feedback is shown in Fig. 4.1(c).
4.2.2 Gyrators
Especially in LC ladders, a gyrator is a useful element because it allows us to convert a capacitor into an inductor, as shown in Fig. 4.2. The characteristic of the gyrator can be described as Also, the voltage across the capacitor C is given by
I sC
V 1
2
2 = × (4.7) From these three equations above, we derive
sL
Fig. 4.2 the Grounded Inductor Implemented by a Gyrator
Moreover, a floating inductor is presented in Fig. 4.3.
Fig. 4.3 the Floating Inductor Realized by a Capacitor between Two Gyrators
4.2.3 Integrators
In this subsection, we introduce the properties of the integrator, which is the fundamental building block of Gm-C filters. To realize an integrator in Gm technology, a transconductor and a capacitor are used as presented in Fig. 4.4.
Fig. 4.4 the Single-ended Integrator
In most integrated applications, the fully differential circuits are common used because they have better noise immunity and distortion properties. Fig. 4.5 presents the fully differential integrators.
Fig. 4.5 the Fully Differential Integrators
At first, we analyze the integrator in Fig. 4.4 for simplicity. In the ideal case, both the input and output impedance of the transconductor are infinite. The transfer function of the integrator can be derived as
sC
On the jω-axis, the equation becomes
)
From the equation (4.10), we can see that the ideal integrator has infinite DC gain.
Besides, quality factor and phase margin are defined as Q(jω)=B(jω) G(jω) and ideal transconductor has infinite quality factor and PM = 90− ° for all frequencies.
Finally, the unity gain frequency for the integrator is
C g
mT
=
ω
(4.11)
As for the non-ideal transconductor, the transfer function includes extra parameters of delay and non-zero conductance G. The delay is caused by the parasitic poles and zeros of transconductor. However, due to the parasitic poles and zeros locating at markedly higher frequency than the unity gain frequency, we could model this circumstance only by one single effective zero. The zero in the right half-plane (RHP) leads to the phase lag. On the other hand, the zero in the left half-plane (LHP) results in the phase lead.
The non-ideal integrator could be modeled as Fig. 4.6. The transfer function of
this non-ideal integrator is
The non-zero conductance causes finite dominate pole and DC gain which is given by
o
Fig. 4.6 the Non-ideal Single-ended Integrator
In Fig. 4.7, the magnitude and phase response of the integrator is given. Normally,
2
1 1
1τ <<ωT << τ
Fig. 4.7 Gain and Phase Response of the Integrator
The parasitic zero and finite DC gain result in the deviation of phase from− 90°. which is a principal error in the filter. By rewriting equation (4.11), the transfer function is
Hence, the quality factor of the integrator can be derived as
))
Qnonideal nonideal ω
ω
According to equation (4.15) and (4.16), the reciprocal value of the quality factor can be described as From the equation (4.17), the quality factor is infinite at the frequency which is the geometric mean of the dominant pole and the effective parasitic zero.
4.3 Fourth-order Equiripple Linear Phase Low-pass Filter
In this section, the 4th order equiripple linear phase filter, cascading by two biquad sections, is presented. This section is divided into three parts. First, we introduce the biquad section. Next, the filter architecture is presented. Finally, output buffers will be discussed.
4.3.1 Biquad Section
The passive RLC circuit of the general impedance converter (GIC) biquad is shown in Fig. 4.8. The transfer function can be expressed in
sC sL
Fig. 4.8 the 2nd Order Bandpass Filter for Passive RLC Prototype
Using the elementary transconductor building block discussed in section 4.2, the active biquad section is shown in Fig. 4.9.
Fig. 4.9 the 2nd Order Bandpass and Lowpass Filter for Active Gm-C Prototype ForR=1 gm2 andL=C2 gm3gm4, the transfer function of bandpass filter is
Using the fact that
The transfer function of lowpass filter is
4 The advantages of the biquad section are the cascade fashion, and the loop is quite stable in high order filter. The disadvantages of the biquad section are the loading effects and the circuit sensitivity, which is more sensitive than LC ladders.
4.3.2 Filter Architecture
The structure of the 4th order linear phase lowpass filter by cascading two biquad sections is shown in Fig. 4.10.
Fig. 4.10 the 4th Order Equiripple Linear Phase Lowpass Filter
Because the output of the first, second and fourth stages in biquad section are connected together, this section only need one common mode feedback circuit,
instead of three, to maintain the output of three stages to the reference voltage.
Moreover, the biquad needs another common mode feedback circuit to maintain the output of the third stage.
From the equation (4.21), the cutoff frequencyω0 and the quality factor Q for a biquad section can be expressed as
C gm1
0 =
ω (4.22)
2 1 m m
g
Q= g (4.23)
= 1
K
(4.24) From the equation (4.22), the unity gain frequency of the first transconductor in the biquad section is equal to the cutoff frequency of the biquad. Table 4.1 presents the denominator of the biquad section and the phase error in the 4th order linear phase filter.TABLE 4.1 Denominator of Biquad Section
As can be seen from the table above, the filter is implemented with 0.05° phase error.
Furthermore, the quality factor and normalized cutoff frequency for the first and second biquads areQ1 =0.5573,ω01=1.0752 Q2 =1.0652,ω02 =1.5865. According to these parameters, the transconductance and capacitance can be designed to fulfill the transfer function.
4.3.3 Output Buffers
While measuring the filter, the loading effect caused by the instruments is a
critical issue. Consequently, using the output buffers to alleviate loading effect is essential. The following presents two methods for realizing the output buffers. One is using a transconductor-based resistor as the output buffer, and the other is using the source follower to implement.
Fig. 4.11 shows the output buffer using transconductor-based resistor. By adding this output buffer, the transfer function becomes
) ( )
( )
( T s T s
V V V V V
s V
T buff filter
i o o obuff i
obuff = × = ×
= (4.25)
To acquire the original transfer function of the filter, we have to divide T(s) by the transfer function of output buffer. However, the output buffer might attenuate the output signal of filter, and thus the signal is too small to be measured.
Fig. 4.11 the Output Buffer Using Transconductor-based Resistor
Another method is using the source follower as the output buffer as presented in Fig. 4.12. Because the gain of the source follower is approximate to 1, it is easy to measure the output signal of source follower without attenuating too much. However, the current in source follower must be large enough to ensure that the DC gain of filter is about 0dB.
Fig. 4.12 the Output Buffer Using Source Follower
Chapter 5
Simulation and Experimental Results
5.1 Introduction
The performances of the OTA and filter are usually expressed as the following parameters, such as CMRR, PSRR, etc. By using these parameters, we can compare the performances with other OTA and filter. In this chapter, the definition of the parameters is introduced. Moreover, the simulation and experimental results of proposed circuits are presented.
Common Mode Rejection Ratio (CMRR):
DM
where ACM-DM denotes common-mode to differential-mode conversion. Large CMRR means that the circuit has a good ability to suppress the effect of common-mode noise.
Power Supply Rejection Ratio (PSRR):
DM
The PSRR is defined as the gain from the input to the output divided by the gain from the supply to the output. The larger the PSRR is, the less the noise from the power supply affects.
Power Consumption or Current Consumption:
The power consumption can be derived from current consumption as
V I
P = ×
(5.3)As mentioned before, the linearity is the main drawback of the Gm-C filter.
There are two parameters, THD and IM3, to describe the linearity performance of the OTA and filters.
Total Harmonic Distortion (THD):
For an ideal OTA, when a single frequency signal applies to the input node, the same frequency signal will show at the output node. However, in practice, the nonlinear effects would cause the harmonic distortion, which means the output signal is composed of the fundamental frequency and harmonic frequencies. By analyzing the output signal, the total harmonic distortion is obtained. The total harmonic distortion of a signal is defined as the total power of the second and higher harmonic frequencies divided by the power of the fundamental signal, as shown below in dB.
⎟⎟
The even harmonic distortion is cancelled due to using fully differential structures.
Furthermore, the high-order harmonic distortions are usually too small to be neglected.
Therefore, the third-order harmonic distortion is a dominant distortion which equals to the THD approximately. The definition is shown in dB as
⎟⎟
In addition, we could use another approach to interpret the HD3. Base on the reasons above, the relation between the input and output can expressed as
)
Assuming the input is a sinusoidal signal as) cos(
)
( t A t
V
in= ω
(5.7)From the equation (5.6) and (5.7), the output signal could be derived as
Third-order Intermodulation (IM3):
While measuring the linearity of the low-pass filter near the edge of passband, the measurement results would be wrong by analyzing with the THD. This is because the high-order harmonic distortions are in the stopband and thus being filtered. As a result, the IM3 is used to measure the filter’s linearity.
The analyzing method with the IM3 is to apply two tone signals as input signal.
)
From equations (5.6) and (5.10), the output signal could be approximately derived as)]
)The output signal of the third and fourth terms might be out of band and thereby being filtered. Nevertheless, the signals of the second term, intermodulation distortions, are close to the input signal. Consequently, we can measure the linearity of the filter by using these properties. The magnitude of the fundamental term and the main intermodulation distortions are given as 1 1 3 3
4 9a A A
a ID = +
and 3 3 3 4 3a A
ID = , respectively. Assuming , the third-order
intermodulation distortion is derived as
4
5.2 Performance of Flipped Voltage Follower OTA with Input Attenuators
5.2.1 Simulation Results of the Transcondutor
In Fig 5.1, the DC gain of the OTA is 42.1dB and the unity gain frequency is 42.7MHz with 86.6∘phase margin.
(a)
(b)
Fig. 5.1 (a) Magnitude Response (b) Phase Response
In Fig. 5.2 and 5.3, the CMRR and PSRR of OTA are 102dB and 69dB at DC, respectively.
Fig. 5.2 the Common Mode Rejection Ratio
Fig. 5.3 the Power Supply Rejection Ratio
In Fig 5.4, the transconductance is varying with different tuning voltage.
Fig. 5.4 the Tuning Range of the OTA
In Fig 5.5, the transcondctance is varying with different frequencies.
Fig. 5.5 the OTA Tuning Range with Highest and Lowest Vtune
In Fig 5.6, the HD3 is about -74dB for 10MHz with 0.8-Vpp input signal.
Fig. 5.6 the Total Harmonic Distortion
5.2.2 Simulation Results of the Filter
From Fig 5.7, the cutoff frequency is about 40MHz, and the group delay is less than 5.4% up to 1.8fc. The maximum value of magnitude response is not 0dB due to the source follower as the output buffer.
(a)
(b)
Fig. 5.7 (a) Magnitude Response (b) Group Delay
In Fig. 5.8 and 5.9, the HD3 is about -60.8dB for 10MHz with 0.8-Vpp input signal and the IM3 is -36.6dB for 39MHz and 41MHz with 0.8-Vpp input signal. The IM3 is normally worse than the HD3, where the IM3= and
HD3= .
) 4 / 3 ( ) /
(a3 a1 × A2 )
4 / ( ) /
(a3 a1 × A2
Fig. 5.8 the Total Harmonic Distortion
Fig. 5.9 the Inter-modulation Distortion TABLE 5.1 the Specification of Filter
5.2.3 Measurement Results of the Filter
The layout for this circuit is shown in Fig. 5.10 (a) and the die photo is shown in Fig. 5.10 (b). The active region is 0.510×0.500mm2.
(a)
(b)
Fig. 5.10 (a) the Layout (b) the Die Photo
The magnitude response and the group delay for the filter are shown in Fig. 5.11.
The cutoff frequency could be tuned from 10MHz to 40MHz and the group delay is about 24ns at the cutoff frequency.
(a)
(b)
Fig. 5.11 (a) Magnitude Response (b) Group Delay
The following measurement results express the linearity performance. The THD is shown in Fig. 5.12. From this figure, the HD3 is -53.4dB at 10MHz for 0.8Vpp
input signal and the HD2 is about -41dB. The second-order harmonic distortion is measured because of the mismatch in the current mirrors and in the input pairs.
Moreover, the mismatch in the off-chip single-ended to differential input and differential output to single-ended conversion setup lead to the distortion as well. In Fig. 5.13, the IM3 is shown to be about -36dB for 39MHz and 41MHz input signals.
Fig. 5.12 the Total Harmonic Distortion
Fig. 5.13 the Inter-modulation Distortion
5.3 Performance of Super Source Follower OTA with a Positive Feedback
5.3.1 Simulation Results of the Transcondutor
In Fig 5.14, the DC gain of the OTA is 36.4dB and the unity gain frequency is 17MHz with 83.8∘phase margin.
(a)
(b)
Fig. 5.14 (a) Magnitude Response (b) Phase Response
In Fig. 5.15 and 5.16, the CMRR and PSRR of OTA are 82dB and 76dB at DC, respectively.
Fig. 5.15 the Common Mode Rejection Ratio
Fig. 5.16 the Power Supply Rejection Ratio
In Fig 5.17, the transconductance is varying with different tuning voltage.
Fig. 5.17 the Tuning Range of the OTA
In Fig 5.18, the transconductance is varying with different frequencies.
Fig. 5.18 the OTA Tuning Range with Highest and Lowest Vtune
In Fig 5.19, the HD3 is about -59dB for 17MHz with 0.6-Vpp input signal.
Fig. 5.19 the Total Harmonic Distortion TABLE 5.2 the Specification of the OTA
5.3.2 Measurement Results of the Transcondutor
The layout for this circuit is shown in Fig. 5.20 (a) and the die photo is shown in Fig. 5.20 (b). The active region is 0.145×0.134mm2.
(a)
(b)
Fig. 5.20 (a) the Layout (b) the Die Photo
The following measurement results express the linearity performance. The THD is shown in Fig. 5.21. From this figure, the HD3 is -69dB at 10MHz for 0.6Vpp input signal and the HD2 is about -64dB. The second-order harmonic distortion is measured because of the mismatch in the current mirrors and in the input pairs. Moreover, the mismatch in the off-chip single-ended to differential input and differential output to single-ended conversion setup lead to the distortion as well. In Fig. 5.22, the IM3 is shown to be about -60dB for 9MHz and 11MHz input signals. Fig. 5.23 shows the HD3 for different frequencies with 0.6-Vpp input signals.
Fig. 5.21 the Total Harmonic Distortion
Fig. 5.22 the Inter-modulation Distortion
Fig. 5.23 the Measured HD3 for Different Frequencies
Table 5.3 summarized this work with recently reported OTAs. In order to compare with other OTAs, the defined figure of merit (FOM), which takes the transconductance value, input swing range, linearity performance, speed of the implemented circuit, and power consumption into consideration, is expressed as follows:
⎟⎟⎠
⎜⎜ ⎞
⎝
⎛ × × ×
= power
f IM
V
FOM Gm id 3linear o
log
10 (5.13)
TABLE 5.3 Comparison of Previously Reported Works
Chapter 6 Conclusions
6.1 Conclusions
When it comes to the high frequencies, the operational transconductance amplifiers (OTAs) have proven to be the best candidate for executing the continuous-time filters. However, because the main drawback of the OTA is poor linearity, the linearity enhancement techniques are required. In this thesis, two approaches of the transconductor for implementing the filter are proposed. The main purpose of the filter is to apply in IEEE 802.11 for the wireless local area networks.
Although the source degeneration circuit can improve the linearity, it is not good enough for some applications. The proposed transconductors are both based on the source degeneration structure and adding extra concepts to implement. One is designed by combining the flipped voltage follower with input attenuators, which is used to achieve the 4th order equiripple linear phase lowpass filter. The measurement result of the filter shows that -36dB IM3 at 40MHz. The other is designed by using the super source follower with a positive feedback to alleviate the non-ideal effects.
For this circuit, the IM3 is shown to be about -60dB at 10MHz.
6.2 Future Works
With the progressing of technology, the power supply voltage will be reduced in nano-scale. In the portable devices, the feature of low power consumption is emphasized especially. As a result, attempting to design in low-voltage low-power with equal or better linearity is a challenge, and it is worthy to do the research.
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