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46 questions set from this chapter, 7 of them more than once. Most asked first.

  • Asked 3 times
  • 2083 Baisakh · 5+4 marks
  • 2080 Bhadra · 8 marks
  • 2074 Chaitra · 4+4 marks

Draw the circuit diagram of Tow-Thomas low pass biquad circuit and derive its transfer function. Design a second order low pass filter using Tow-Thomas biquad with poles at -450 ± j893.03 and dc gain of 1.5. The final circuit should contain practically realizable elements.

Answer

Tow-Thomas low-pass biquad

The Tow-Thomas biquad is a two-integrator-loop circuit using three op-amps: a lossy integrator, an ideal integrator and an inverter in a feedback loop. It gives low-pass and band-pass outputs at the same time, has low sensitivity, and lets ω0\omega_0, QQ and gain be tuned independently.

            R1 (sets Q)
          +--/\/\--+
          |   C1   |
          +---||---+
          |        |
Vin--R4---+--[OA1]-+--> V1 (band-pass)
          ^
          |  V1--R3-->[OA2 integrator, C2]--> V2 (LP)
          |  V2--r--->[OA3 inverter, r/r]---> V3=-V2
          |                                    |
          +------------------R2----------------+

All op-amp (+) inputs are grounded. OA1 is a lossy integrator (R1∥C1R_1 \parallel C_1 in feedback), OA2 an ideal integrator (C2C_2 in feedback), OA3 a unity-gain inverter.

Derivation (ideal op-amps, so each inverting input is a virtual ground):

KCL at the inverting input of OA1:

VinR4+V3R2+V1(1R1+sC1)=0\frac{V_{in}}{R_4} + \frac{V_3}{R_2} + V_1\left(\frac{1}{R_1} + sC_1\right) = 0

OA2 (integrator) and OA3 (inverter):

V2=−V1sR3C2,V3=−V2=V1sR3C2  ⇒  V1=sR3C2V3V_2 = -\frac{V_1}{sR_3C_2}, \qquad V_3 = -V_2 = \frac{V_1}{sR_3C_2} \;\Rightarrow\; V_1 = sR_3C_2V_3

Substituting V1V_1 into the KCL equation:

sR3C2V3(1R1+sC1)+V3R2=−VinR4V3(s2R3C1C2+sR3C2R1+1R2)=−VinR4\begin{aligned} sR_3C_2V_3\left(\frac{1}{R_1} + sC_1\right) + \frac{V_3}{R_2} &= -\frac{V_{in}}{R_4} \\ V_3\left(s^2R_3C_1C_2 + \frac{sR_3C_2}{R_1} + \frac{1}{R_2}\right) &= -\frac{V_{in}}{R_4} \end{aligned}

Dividing by R3C1C2R_3C_1C_2:

V3Vin=−1R3R4C1C2s2+sR1C1+1R2R3C1C2,V2Vin=−V3Vin\frac{V_3}{V_{in}} = \frac{-\dfrac{1}{R_3R_4C_1C_2}}{s^2 + \dfrac{s}{R_1C_1} + \dfrac{1}{R_2R_3C_1C_2}}, \qquad \frac{V_2}{V_{in}} = -\frac{V_3}{V_{in}}

Comparing with T(s)=±Kω02s2+(ω0/Q)s+ω02T(s) = \dfrac{\pm K\omega_0^2}{s^2 + (\omega_0/Q)s + \omega_0^2}:

ω0=1R2R3C1C2,ω0Q=1R1C1,K=R2R4 (dc gain)\omega_0 = \frac{1}{\sqrt{R_2R_3C_1C_2}}, \qquad \frac{\omega_0}{Q} = \frac{1}{R_1C_1}, \qquad K = \frac{R_2}{R_4}\ \text{(dc gain)}

V2V_2 is a non-inverting low-pass output and V3V_3 an inverting one; V1V_1 is a band-pass output.

Design

Step 1: ω0\omega_0 and QQ from the poles. Poles s=−σ±jωds = -\sigma \pm j\omega_d with σ=450\sigma = 450, ωd=893.03\omega_d = 893.03:

ω02=σ2+ωd2=4502+893.032=1,000,002.6  ⇒  ω0≈1000 rad/sω0Q=2σ  ⇒  Q=ω02σ=1000900=1.111\begin{aligned} \omega_0^2 &= \sigma^2 + \omega_d^2 = 450^2 + 893.03^2 = 1{,}000{,}002.6 \;\Rightarrow\; \omega_0 \approx 1000\ \text{rad/s} \\ \frac{\omega_0}{Q} &= 2\sigma \;\Rightarrow\; Q = \frac{\omega_0}{2\sigma} = \frac{1000}{900} = 1.111 \end{aligned}

Required transfer function (dc gain K=1.5K = 1.5):

T(s)=1.5 ω02s2+2σs+ω02=1.5×106s2+900 s+106T(s) = \frac{1.5\,\omega_0^2}{s^2 + 2\sigma s + \omega_0^2} = \frac{1.5 \times 10^{6}}{s^2 + 900\,s + 10^{6}}

Design equations (choose C1=C2=CC_1 = C_2 = C, R2=R3=RR_2 = R_3 = R):

R=1ω0C,R1=QR=Qω0C,R4=R2K,r=any convenient valueR = \frac{1}{\omega_0 C}, \qquad R_1 = QR = \frac{Q}{\omega_0 C}, \qquad R_4 = \frac{R_2}{K}, \qquad r = \text{any convenient value}

Step 2: Element values. Choose C1=C2=C=0.1 μC_1 = C_2 = C = 0.1\ \muF (a standard value that gives resistors in the kΩ\Omega range).

R2=R3=R=1ω0C=11000×0.1×10−6=10 kΩR1=QR=1.111×10 kΩ=11.11 kΩR4=R2K=10 kΩ1.5=6.667 kΩr=10 kΩ (inverter, equal resistors)\begin{aligned} R_2 = R_3 = R &= \frac{1}{\omega_0 C} = \frac{1}{1000 \times 0.1\times10^{-6}} = 10\ \text{k}\Omega \\ R_1 &= QR = 1.111 \times 10\ \text{k}\Omega = 11.11\ \text{k}\Omega \\ R_4 &= \frac{R_2}{K} = \frac{10\ \text{k}\Omega}{1.5} = 6.667\ \text{k}\Omega \\ r &= 10\ \text{k}\Omega \ \text{(inverter, equal resistors)} \end{aligned}

Final circuit: Tow-Thomas biquad (figure above) with C1=C2=0.1 μFC_1 = C_2 = 0.1\ \mu\text{F}, R1=11.11 kΩR_1 = 11.11\ \text{k}\Omega, R2=R3=10 kΩR_2 = R_3 = 10\ \text{k}\Omega, R4=6.667 kΩR_4 = 6.667\ \text{k}\Omega, r=10 kΩr = 10\ \text{k}\Omega; take the output at V2V_2 (OA2 output) for a positive dc gain of 1.5.

Answer: C=0.1 μFC = 0.1\ \mu\text{F}, R1=11.11 kΩR_1 = 11.11\ \text{k}\Omega, R2=R3=10 kΩR_2 = R_3 = 10\ \text{k}\Omega, R4=6.667 kΩR_4 = 6.667\ \text{k}\Omega, r=10 kΩr = 10\ \text{k}\Omega (all practical values).

  • Asked 3 times
  • 2080 Baisakh · 5 marks
  • 2074 Chaitra · 5 marks
  • 2082 Chaitra (new course) · 7 marks

How can excess gain be compensated in Sallen-Key circuit? Explain with necessary derivations and diagrams.

Answer

In the equal-component Sallen-Key low-pass design the amplifier gain is fixed by the required QQ: K=3−1/QK = 3 - 1/Q. The filter's dc gain therefore equals KK, which is often more than the gain wanted. The excess gain is removed without disturbing ω0\omega_0 and QQ by replacing the input resistor R1R_1 with a voltage divider (gain reduction).

Sallen-Key low-pass circuit

                 C1
          +------||------------+
          |                    |
Vin--R1---+A--R2--+B---(+)     |
                  |     OA >---+--- Vo
                 C2  +-(-)     |
                  |  |         RB
                 GND +---------+
                     |
                     RA
                     |
                    GND

Amplifier gain K=1+RB/RAK = 1 + R_B/R_A, so VB=Vo/KV_B = V_o/K.

Derivation. Node B: VA−VBR2=sC2VB⇒VA=VB(1+sR2C2)\dfrac{V_A - V_B}{R_2} = sC_2V_B \Rightarrow V_A = V_B(1 + sR_2C_2).

Node A:

Vin−VAR1=VA−VBR2+sC1(VA−Vo),VB=VoK\frac{V_{in} - V_A}{R_1} = \frac{V_A - V_B}{R_2} + sC_1(V_A - V_o), \quad V_B = \frac{V_o}{K}

Eliminating VAV_A and VBV_B:

T(s)=VoVin=KR1R2C1C2s2+s(1R1C1+1R2C1+1−KR2C2)+1R1R2C1C2T(s) = \frac{V_o}{V_{in}} = \frac{\dfrac{K}{R_1R_2C_1C_2}}{s^2 + s\left(\dfrac{1}{R_1C_1} + \dfrac{1}{R_2C_1} + \dfrac{1-K}{R_2C_2}\right) + \dfrac{1}{R_1R_2C_1C_2}}

so ω0=1R1R2C1C2\omega_0 = \dfrac{1}{\sqrt{R_1R_2C_1C_2}} and ω0Q=1R1C1+1R2C1+1−KR2C2\dfrac{\omega_0}{Q} = \dfrac{1}{R_1C_1} + \dfrac{1}{R_2C_1} + \dfrac{1-K}{R_2C_2}. For the equal-component design (R1=R2=RR_1 = R_2 = R, C1=C2=CC_1 = C_2 = C): ω0=1/RC\omega_0 = 1/RC and ω0/Q=(3−K)/RC\omega_0/Q = (3-K)/RC, so K=3−1/QK = 3 - 1/Q.

Compensation by input voltage divider

Suppose the required gain is H<KH < K. Replace R1R_1 by two resistors R1aR_{1a} (series) and R1bR_{1b} (to ground):

Vin--R1a--+--> node A        Thevenin equivalent:
          |                  Vth = alpha*Vin
         R1b                 Rth = R1a || R1b = R1
          |
         GND

The Thevenin equivalent seen from node A is a source αVin\alpha V_{in} in series with R1a∥R1bR_{1a}\parallel R_{1b}, where

α=R1bR1a+R1b,R1a∥R1b=R1aR1bR1a+R1b\alpha = \frac{R_{1b}}{R_{1a} + R_{1b}}, \qquad R_{1a}\parallel R_{1b} = \frac{R_{1a}R_{1b}}{R_{1a}+R_{1b}}

If we make R1a∥R1b=R1R_{1a}\parallel R_{1b} = R_1, the network seen by node A is unchanged, so ω0\omega_0 and QQ are unchanged, and the transfer function becomes

VoVin=α T(s)  ⇒  dc gain=αK=H  ⇒  α=HK\frac{V_o}{V_{in}} = \alpha\,T(s) \;\Rightarrow\; \text{dc gain} = \alpha K = H \;\Rightarrow\; \alpha = \frac{H}{K}

Solving the two conditions:

R1a=R1α,R1b=R11−αR_{1a} = \frac{R_1}{\alpha}, \qquad R_{1b} = \frac{R_1}{1-\alpha}

Check: R1a∥R1b=R12/[α(1−α)]R1/[α(1−α)]=R1R_{1a}\parallel R_{1b} = \dfrac{R_1^2/[\alpha(1-\alpha)]}{R_1/[\alpha(1-\alpha)]} = R_1.

Example

For a 2nd order Butterworth filter (Q=0.7071Q = 0.7071), K=3−1.414=1.586K = 3 - 1.414 = 1.586. For unity overall gain (H=1H = 1): α=1/1.586=0.6306\alpha = 1/1.586 = 0.6306, so R1a=R1/0.6306=1.586R1R_{1a} = R_1/0.6306 = 1.586R_1 and R1b=R1/0.3694=2.707R1R_{1b} = R_1/0.3694 = 2.707R_1. With R1=10R_1 = 10 kΩ\Omega: R1a=15.86R_{1a} = 15.86 kΩ\Omega, R1b=27.07R_{1b} = 27.07 kΩ\Omega.

Notes

  • Only the input resistor changes; C1C_1, C2C_2, R2R_2 and the gain resistors RAR_A, RBR_B stay the same.
  • This method can only reduce gain (α<1\alpha < 1). If more gain is needed, gain enhancement (feeding C1C_1 from a tap of an output divider) or a separate amplifier stage is used.
  • Asked 3 times
  • 2079 Baisakh · 4 marks
  • 2073 Shrawan · 5 marks
  • 2071 Shrawan · 5 marks

How can the gain enhancement be performed in a Sallen-Key circuit? Explain with necessary diagram.

Answer

In the equal-component Sallen-Key low-pass filter the amplifier gain is fixed by QQ (K=3−1/QK = 3 - 1/Q), so the dc gain is fixed too. Gain enhancement raises the overall gain above KK while keeping ω0\omega_0 and QQ unchanged.

Basic idea

The RC network only "sees" the voltage that is fed back through C1C_1 and the voltage at the (+) input. If the op-amp output is made larger by a factor 1/β1/\beta, but only βVo\beta V_o is fed back to C1C_1 (and set as KK times VBV_B), the RC network works exactly as before while the output is bigger.

Circuit

              C1
          +---||-------------------+
          |                        |
Vin--R1---+A--R2--+B--(+)          |
                  |     OA(mu)--+--|--- Vo
                 C2             |  |
                  |             Rc |
                 GND            +--+ Vo' = beta*Vo
                                |
                                Rd
                                |
                               GND
 OA(mu): non-inverting amp, mu = 1 + RB/RA

The op-amp output VoV_o drives a divider RcR_c, RdR_d; capacitor C1C_1 is returned to the tap Vo′=βVoV_o' = \beta V_o where β=RdRc+Rd<1\beta = \dfrac{R_d}{R_c + R_d} < 1 (the divider resistance Rc∥RdR_c\parallel R_d is made small compared with the impedance of C1C_1, or absorbed into the design).

Derivation

Let the non-inverting amplifier gain be μ=1+RB/RA\mu = 1 + R_B/R_A, so Vo=μVBV_o = \mu V_B and Vo′=βμVBV_o' = \beta\mu V_B. The RC network now sees an "effective gain" βμ\beta\mu from node B to the point where C1C_1 returns. Writing the node equations exactly as for the normal circuit with VoV_o replaced by Vo′V_o':

Vo′Vin=βμR1R2C1C2s2+s(1R1C1+1R2C1+1−βμR2C2)+1R1R2C1C2\frac{V_o'}{V_{in}} = \frac{\dfrac{\beta\mu}{R_1R_2C_1C_2}}{s^2 + s\left(\dfrac{1}{R_1C_1} + \dfrac{1}{R_2C_1} + \dfrac{1-\beta\mu}{R_2C_2}\right) + \dfrac{1}{R_1R_2C_1C_2}}

For the required QQ, set βμ=K=3−1/Q\beta\mu = K = 3 - 1/Q (equal-component case). Then ω0\omega_0 and QQ are the same as before, and the output is

VoVin=1β⋅Vo′Vin  ⇒  dc gain=Kβ>K\frac{V_o}{V_{in}} = \frac{1}{\beta}\cdot\frac{V_o'}{V_{in}} \;\Rightarrow\; \text{dc gain} = \frac{K}{\beta} > K

Design steps

  1. Design the normal equal-component Sallen-Key for ω0\omega_0 and QQ; this gives K=3−1/QK = 3 - 1/Q.
  2. For a required dc gain H>KH > K, choose β=K/H\beta = K/H.
  3. Set the op-amp gain μ=1+RB/RA=H\mu = 1 + R_B/R_A = H and choose the divider Rd/(Rc+Rd)=βR_d/(R_c+R_d) = \beta.

Example: Butterworth (Q=0.707Q = 0.707, K=1.586K = 1.586) with required gain H=5H = 5: β=1.586/5=0.317\beta = 1.586/5 = 0.317, μ=5\mu = 5 (RB=4RAR_B = 4R_A), and the divider is Rc=2.15RdR_c = 2.15R_d (e.g. Rd=1R_d = 1 kΩ\Omega, Rc=2.15R_c = 2.15 kΩ\Omega).

For gain reduction (the opposite case) the input resistor R1R_1 is split into a voltage divider instead.

  • Asked 3 times
  • 2081 Baisakh · 4 marks
  • 2078 Bhadra · 5 marks
  • 2072 Kartik · 4 marks

Design an active filter using non-inverting op-amp configuration with following transfer function. T(s) = (s+8)/(s+2)

Answer

Approach

A non-inverting op-amp amplifier with impedance Z1Z_1 from the (-) input to ground and Z2Z_2 in feedback has

T(s)=1+Z2Z1T(s) = 1 + \frac{Z_2}{Z_1}
Vin ---------(+)
                \
                 OA >----+---- Vo
                /        |
     +-------(-)         |
     |                   |
     +-------[ Z2 ]------+
     |
   [ Z1 ]
     |
    GND

Matching the given function

T(s)=s+8s+2=1+6s+2  ⇒  Z2Z1=6s+2T(s) = \frac{s+8}{s+2} = 1 + \frac{6}{s+2} \;\Rightarrow\; \frac{Z_2}{Z_1} = \frac{6}{s+2}

Take Z1=R1Z_1 = R_1 and Z2=R2∥CZ_2 = R_2 \parallel C:

Z2=R21+sR2C=1/Cs+1/(R2C),Z2Z1=1/(R1C)s+1/(R2C)Z_2 = \frac{R_2}{1 + sR_2C} = \frac{1/C}{s + 1/(R_2C)}, \qquad \frac{Z_2}{Z_1} = \frac{1/(R_1C)}{s + 1/(R_2C)}

Comparing:

1R2C=2,1R1C=6\frac{1}{R_2C} = 2, \qquad \frac{1}{R_1C} = 6

Normalized values (C=1C = 1 F): R2=0.5 ΩR_2 = 0.5\ \Omega, R1=1/6=0.1667 ΩR_1 = 1/6 = 0.1667\ \Omega.

Check: T(s)=1+6s+2=s+8s+2T(s) = 1 + \dfrac{6}{s+2} = \dfrac{s+8}{s+2}. Zero at s=−8s = -8, pole at s=−2s = -2, dc gain 8/2=48/2 = 4, high-frequency gain 1.

Practical values (impedance scaling)

Choose C=1 μC = 1\ \muF, i.e. km=106k_m = 10^6 (frequencies unchanged):

R2=0.5×106=500 kΩ,R1=0.1667×106=166.7 kΩ,C=1 μFR_2 = 0.5 \times 10^6 = 500\ \text{k}\Omega, \qquad R_1 = 0.1667\times10^6 = 166.7\ \text{k}\Omega, \qquad C = 1\ \mu\text{F}

Answer: non-inverting amplifier with R1=166.7R_1 = 166.7 kΩ\Omega to ground and R2=500R_2 = 500 kΩ\Omega in parallel with C=1 μC = 1\ \muF in feedback (normalized: R1=1/6 ΩR_1 = 1/6\ \Omega, R2=0.5 ΩR_2 = 0.5\ \Omega, C=1C = 1 F). A non-inverting stage can only realize ∣T∣≥1|T| \ge 1 forms like this one (zero farther from the origin than the pole).

  • Asked 2 times
  • 2076 Chaitra · 4+4 marks
  • 2075 Chaitra · 4+4 marks

Derive the transfer function of Sallen-Key low pass filter. Design a filter for T(s) = 1/(s² + 0.765s + 1) using Sallen-Key biquad. In your final design the values of capacitors must be 0.01μF and feedback resistors should be equal.

Answer

Sallen-Key low-pass biquad

The Sallen-Key (positive-feedback, VCVS) biquad uses one op-amp as a non-inverting amplifier of gain KK with an RC network.

                 C1
          +------||------------+
          |                    |
Vin--R1---+A--R2--+B---(+)     |
                  |     OA >---+--- Vo
                 C2  +-(-)     |
                  |  |         RB
                 GND +---------+
                     |
                     RA
                     |
                    GND

Amplifier gain K=1+RB/RAK = 1 + R_B/R_A, so VB=Vo/KV_B = V_o/K.

Derivation. Node B: VA−VBR2=sC2VB⇒VA=VB(1+sR2C2)\dfrac{V_A - V_B}{R_2} = sC_2V_B \Rightarrow V_A = V_B(1 + sR_2C_2).

Node A:

Vin−VAR1=VA−VBR2+sC1(VA−Vo),VB=VoK\frac{V_{in} - V_A}{R_1} = \frac{V_A - V_B}{R_2} + sC_1(V_A - V_o), \quad V_B = \frac{V_o}{K}

Eliminating VAV_A and VBV_B:

T(s)=VoVin=KR1R2C1C2s2+s(1R1C1+1R2C1+1−KR2C2)+1R1R2C1C2T(s) = \frac{V_o}{V_{in}} = \frac{\dfrac{K}{R_1R_2C_1C_2}}{s^2 + s\left(\dfrac{1}{R_1C_1} + \dfrac{1}{R_2C_1} + \dfrac{1-K}{R_2C_2}\right) + \dfrac{1}{R_1R_2C_1C_2}}

so ω0=1R1R2C1C2\omega_0 = \dfrac{1}{\sqrt{R_1R_2C_1C_2}} and ω0Q=1R1C1+1R2C1+1−KR2C2\dfrac{\omega_0}{Q} = \dfrac{1}{R_1C_1} + \dfrac{1}{R_2C_1} + \dfrac{1-K}{R_2C_2}. For the equal-component design (R1=R2=RR_1 = R_2 = R, C1=C2=CC_1 = C_2 = C): ω0=1/RC\omega_0 = 1/RC and ω0/Q=(3−K)/RC\omega_0/Q = (3-K)/RC, so K=3−1/QK = 3 - 1/Q.

Design for T(s)=1s2+0.765s+1T(s) = \dfrac{1}{s^2 + 0.765s + 1}

Interpretation: "feedback resistors equal" is taken as the equal-resistor (R1=R2R_1 = R_2) equal-capacitor design with C=0.01 μC = 0.01\ \muF.

Step 1: Parameters.

ω02=1⇒ω0=1 rad/s,ω0Q=0.765⇒Q=10.765=1.307\omega_0^2 = 1 \Rightarrow \omega_0 = 1\ \text{rad/s}, \qquad \frac{\omega_0}{Q} = 0.765 \Rightarrow Q = \frac{1}{0.765} = 1.307

Step 2: Amplifier gain.

K=3−1Q=3−0.765=2.235,1+RBRA=2.235⇒RB=1.235RAK = 3 - \frac{1}{Q} = 3 - 0.765 = 2.235, \qquad 1 + \frac{R_B}{R_A} = 2.235 \Rightarrow R_B = 1.235R_A

Choose RA=10R_A = 10 kΩ\Omega, RB=12.35R_B = 12.35 kΩ\Omega.

Step 3: Normalized design. C1=C2=1C_1 = C_2 = 1 F, R1=R2=1 ΩR_1 = R_2 = 1\ \Omega gives ω0=1\omega_0 = 1 and ω0/Q=(3−K)/1=0.765\omega_0/Q = (3-K)/1 = 0.765.

Step 4: Impedance scaling to C=0.01 μC = 0.01\ \muF: km=1C ω0=110−8×1=108k_m = \dfrac{1}{C\,\omega_0} = \dfrac{1}{10^{-8} \times 1} = 10^8.

R1=R2=1ω0C=11×0.01×10−6=100 MΩR_1 = R_2 = \frac{1}{\omega_0 C} = \frac{1}{1 \times 0.01\times10^{-6}} = 100\ \text{M}\Omega

Because the given T(s)T(s) is normalized (ω0=1\omega_0 = 1 rad/s), the resistors come out very large. For a practical cutoff, the same design is frequency scaled; e.g. for ω0=104\omega_0 = 10^4 rad/s, R1=R2=1/(104×10−8)=10R_1 = R_2 = 1/(10^4 \times 10^{-8}) = 10 kΩ\Omega with the same capacitors and the same KK.

Step 5: Gain. The dc gain of this circuit is K=2.235K = 2.235. The given T(s)T(s) has unity dc gain, so the excess gain is removed by splitting R1R_1 into a divider: α=1/2.235=0.4474\alpha = 1/2.235 = 0.4474, R1a=R1/α=2.235R1R_{1a} = R_1/\alpha = 2.235R_1, R1b=R1/(1−α)=1.810R1R_{1b} = R_1/(1-\alpha) = 1.810R_1.

Answer: C1=C2=0.01 μC_1 = C_2 = 0.01\ \muF, R1=R2=100R_1 = R_2 = 100 MΩ\Omega (for ω0=1\omega_0 = 1 rad/s; 10 kΩ\Omega if scaled to 10410^4 rad/s), K=2.235K = 2.235 (RA=10R_A = 10 kΩ\Omega, RB=12.35R_B = 12.35 kΩ\Omega); for unity gain, R1R_1 is replaced by R1a=2.235R1R_{1a} = 2.235R_1 and R1b=1.810R1R_{1b} = 1.810R_1.

  • Asked 2 times
  • 2075 Asoj · 4 marks
  • 2070 Chaitra · 4 marks

What is RC-CR transformation? How can you convert a Sallen Key low pass filter into the Sallen Key High pass filter using RC-CR transformation? (Draw the circuit diagram of the high pass Sallen-Key biquad so obtained.)

Answer

RC-CR transformation converts an active RC low-pass filter into a high-pass filter of the same order and ω0\omega_0 by replacing every resistor (of the frequency-determining RC network) by a capacitor and every capacitor by a resistor. In normalized form, Ri→Ci=1/RiR_i \to C_i = 1/R_i and Cj→Rj=1/CjC_j \to R_j = 1/C_j. This is equivalent to the LP to HP transformation s→1/ss \to 1/s, because the impedance RR becomes 1/(sC)1/(sC) and 1/(sC)1/(sC) becomes RR. Resistors that set the amplifier gain (RAR_A, RBR_B) are not changed, since they do not depend on frequency.

Applying it to the Sallen-Key LPF

Sallen-Key LPF: R1R_1, R2R_2 in series path, C1C_1 feedback to output, C2C_2 to ground, gain KK:

TLP(s)=K/(R1R2C1C2)s2+s(1R1C1+1R2C1+1−KR2C2)+1R1R2C1C2T_{LP}(s) = \frac{K/(R_1R_2C_1C_2)}{s^2 + s\left(\frac{1}{R_1C_1} + \frac{1}{R_2C_1} + \frac{1-K}{R_2C_2}\right) + \frac{1}{R_1R_2C_1C_2}}

After RC-CR: the series elements become capacitors C1C_1, C2C_2; the feedback element and the grounded element become resistors R1R_1 (to output) and R2R_2 (to ground).

                 R1
          +-----/\/\-----------+
          |                    |
Vin--C1---+A--C2--+B---(+)     |
                  |     OA >---+--- Vo
                 R2  +-(-)     |
                  |  |         RB
                 GND +---------+
                     RA
                     |
                    GND

Analysing this circuit gives

THP(s)=Ks2s2+s(1R2C1+1R2C2+1−KR1C1)+1R1R2C1C2T_{HP}(s) = \frac{Ks^2}{s^2 + s\left(\frac{1}{R_2C_1} + \frac{1}{R_2C_2} + \frac{1-K}{R_1C_1}\right) + \frac{1}{R_1R_2C_1C_2}}

For equal components (R1=R2=RR_1 = R_2 = R, C1=C2=CC_1 = C_2 = C): ω0=1/RC\omega_0 = 1/RC, ω0/Q=(3−K)/RC\omega_0/Q = (3-K)/RC (same as the LPF) and high-frequency gain KK. So a normalized LPF with C=1C = 1 F, R=1 ΩR = 1\ \Omega becomes an HPF with R=1 ΩR = 1\ \Omega, C=1C = 1 F at the same ω0\omega_0 and QQ.

  • Asked 2 times
  • 2072 Chaitra · 5 marks
  • 2079 Bhadra · 6 marks

Realize the following transfer function by cascading two first-order sections using inverting op-amp configuration. T(s) = 12/(s² + 8s + 12)

Answer

Factorize

T(s)=12s2+8s+12=12(s+2)(s+6)=(−2s+2)⏟T1(−6s+6)⏟T2T(s) = \frac{12}{s^2+8s+12} = \frac{12}{(s+2)(s+6)} = \underbrace{\left(\frac{-2}{s+2}\right)}_{T_1}\underbrace{\left(\frac{-6}{s+6}\right)}_{T_2}

Each factor is an inverting first-order low-pass section; the two minus signs cancel, giving the required positive sign. (Each section has dc gain −1-1, so the total dc gain is 12/12=112/12 = 1.)

First-order inverting section

            +---[ R2 ]---+
            +---| C |----+
            |            |
Vin--R1-----+--(-)       |
                  OA >---+--- Vo
           GND--(+)
T(s)=−ZfR1=−R2/(1+sR2C)R1=−1/(R1C)s+1/(R2C)T(s) = -\frac{Z_f}{R_1} = -\frac{R_2/(1+sR_2C)}{R_1} = -\frac{1/(R_1C)}{s + 1/(R_2C)}

Section 1: T1=−2s+2T_1 = -\dfrac{2}{s+2}

1/(R2C)=21/(R_2C) = 2 and 1/(R1C)=21/(R_1C) = 2. Normalized (C=1C = 1 F): R1=R2=0.5 ΩR_1 = R_2 = 0.5\ \Omega.

Section 2: T2=−6s+6T_2 = -\dfrac{6}{s+6}

1/(R2C)=61/(R_2C) = 6 and 1/(R1C)=61/(R_1C) = 6. Normalized (C=1C = 1 F): R1=R2=1/6=0.1667 ΩR_1 = R_2 = 1/6 = 0.1667\ \Omega.

Practical values

Impedance scale by km=106k_m = 10^6 (choose C=1 μC = 1\ \muF in both sections):

SectionR1R_1R2R_2CCPole
1500 kΩ\Omega500 kΩ\Omega1 μ\muFs=−2s = -2
2166.7 kΩ\Omega166.7 kΩ\Omega1 μ\muFs=−6s = -6

Cascade

Vin-->[ Section 1: -2/(s+2) ]-->[ Section 2: -6/(s+6) ]--> Vo

Op-amp outputs have very low output impedance, so the sections do not load each other and the overall transfer function is the product:

T(s)=−2s+2⋅−6s+6=12s2+8s+12T(s) = \frac{-2}{s+2}\cdot\frac{-6}{s+6} = \frac{12}{s^2+8s+12}

Answer: two inverting first-order sections in cascade: R1=R2=500R_1 = R_2 = 500 kΩ\Omega, C=1 μC = 1\ \muF (pole at 2 rad/s), and R1=R2=166.7R_1 = R_2 = 166.7 kΩ\Omega, C=1 μC = 1\ \muF (pole at 6 rad/s).

  • 2080 Bhadra · 8 marks

Draw the circuit diagram of Tow-Thomas high pass biquad circuit and derive transfer function. Design a low pass filter using Tow Thomas Biquad circuit with poles at -450 ± j893.03 and dc gain of 1.5. Your final circuit contain practically realizable elements.

Answer

Tow-Thomas high-pass biquad

The basic Tow-Thomas loop (lossy integrator OA1, integrator OA2, inverter OA3) gives LP and BP outputs. A high-pass output is obtained by feeding the input to OA1 through a capacitor CfC_f instead of the resistor R4R_4; the output is taken at OA1.

            R1
          +--/\/\--+
          |   C1   |
          +---||---+
          |        |
Vin--Cf---+--[OA1]-+--> V1 (high-pass output)
          ^
          |  V1--R3-->[OA2 integrator, C2]--> V2
          |  V2--r--->[OA3 inverter, r/r]---> V3=-V2
          |                                    |
          +------------------R2----------------+

Derivation. KCL at OA1's inverting input (virtual ground):

sCfVin+V3R2+V1(1R1+sC1)=0sC_fV_{in} + \frac{V_3}{R_2} + V_1\left(\frac{1}{R_1} + sC_1\right) = 0

From OA2 and OA3: V3=−V2=V1sR3C2V_3 = -V_2 = \dfrac{V_1}{sR_3C_2}. Substituting:

V1(sC1+1R1+1sR2R3C2)=−sCfVinV_1\left(sC_1 + \frac{1}{R_1} + \frac{1}{sR_2R_3C_2}\right) = -sC_fV_{in}

Multiplying by s/C1s/C_1:

V1Vin=−CfC1s2s2+sR1C1+1R2R3C1C2\frac{V_1}{V_{in}} = \frac{-\dfrac{C_f}{C_1}s^2}{s^2 + \dfrac{s}{R_1C_1} + \dfrac{1}{R_2R_3C_1C_2}}

This is a second-order high-pass function with ω0=1/R2R3C1C2\omega_0 = 1/\sqrt{R_2R_3C_1C_2}, ω0/Q=1/(R1C1)\omega_0/Q = 1/(R_1C_1) and high-frequency gain −Cf/C1-C_f/C_1.

Low-pass Tow-Thomas used for the design

With the resistor R4R_4 at the input (figure above with CfC_f replaced by R4R_4), the same analysis gives at V2V_2:

V2Vin=1R3R4C1C2s2+sR1C1+1R2R3C1C2,ω0=1R2R3C1C2, ω0Q=1R1C1, K=R2R4\frac{V_2}{V_{in}} = \frac{\dfrac{1}{R_3R_4C_1C_2}}{s^2 + \dfrac{s}{R_1C_1} + \dfrac{1}{R_2R_3C_1C_2}}, \quad \omega_0 = \frac{1}{\sqrt{R_2R_3C_1C_2}},\ \frac{\omega_0}{Q} = \frac{1}{R_1C_1},\ K = \frac{R_2}{R_4}

Design

Step 1: ω0\omega_0 and QQ from the poles. Poles s=−σ±jωds = -\sigma \pm j\omega_d with σ=450\sigma = 450, ωd=893.03\omega_d = 893.03:

ω02=σ2+ωd2=4502+893.032=1,000,002.6  ⇒  ω0≈1000 rad/sω0Q=2σ  ⇒  Q=ω02σ=1000900=1.111\begin{aligned} \omega_0^2 &= \sigma^2 + \omega_d^2 = 450^2 + 893.03^2 = 1{,}000{,}002.6 \;\Rightarrow\; \omega_0 \approx 1000\ \text{rad/s} \\ \frac{\omega_0}{Q} &= 2\sigma \;\Rightarrow\; Q = \frac{\omega_0}{2\sigma} = \frac{1000}{900} = 1.111 \end{aligned}

Required transfer function (dc gain K=1.5K = 1.5):

T(s)=1.5 ω02s2+2σs+ω02=1.5×106s2+900 s+106T(s) = \frac{1.5\,\omega_0^2}{s^2 + 2\sigma s + \omega_0^2} = \frac{1.5 \times 10^{6}}{s^2 + 900\,s + 10^{6}}

Design equations (choose C1=C2=CC_1 = C_2 = C, R2=R3=RR_2 = R_3 = R):

R=1ω0C,R1=QR=Qω0C,R4=R2K,r=any convenient valueR = \frac{1}{\omega_0 C}, \qquad R_1 = QR = \frac{Q}{\omega_0 C}, \qquad R_4 = \frac{R_2}{K}, \qquad r = \text{any convenient value}

Step 2: Element values. Choose C1=C2=C=0.1 μC_1 = C_2 = C = 0.1\ \muF (a standard value that gives resistors in the kΩ\Omega range).

R2=R3=R=1ω0C=11000×0.1×10−6=10 kΩR1=QR=1.111×10 kΩ=11.11 kΩR4=R2K=10 kΩ1.5=6.667 kΩr=10 kΩ (inverter, equal resistors)\begin{aligned} R_2 = R_3 = R &= \frac{1}{\omega_0 C} = \frac{1}{1000 \times 0.1\times10^{-6}} = 10\ \text{k}\Omega \\ R_1 &= QR = 1.111 \times 10\ \text{k}\Omega = 11.11\ \text{k}\Omega \\ R_4 &= \frac{R_2}{K} = \frac{10\ \text{k}\Omega}{1.5} = 6.667\ \text{k}\Omega \\ r &= 10\ \text{k}\Omega \ \text{(inverter, equal resistors)} \end{aligned}

Final circuit: Tow-Thomas biquad (figure above) with C1=C2=0.1 μFC_1 = C_2 = 0.1\ \mu\text{F}, R1=11.11 kΩR_1 = 11.11\ \text{k}\Omega, R2=R3=10 kΩR_2 = R_3 = 10\ \text{k}\Omega, R4=6.667 kΩR_4 = 6.667\ \text{k}\Omega, r=10 kΩr = 10\ \text{k}\Omega; take the output at V2V_2 (OA2 output) for a positive dc gain of 1.5.

Answer: C=0.1 μFC = 0.1\ \mu\text{F}, R1=11.11 kΩR_1 = 11.11\ \text{k}\Omega, R2=R3=10 kΩR_2 = R_3 = 10\ \text{k}\Omega, R4=6.667 kΩR_4 = 6.667\ \text{k}\Omega, r=10 kΩr = 10\ \text{k}\Omega (all practical values).

  • 2082 Chaitra (new course) · 3+5 marks

Draw the circuit diagram of Tow-Thomas biquad circuit and derive its transfer function. For an ECG machine of a hospital, you are asked to design a low pass filter using Tow-Thomas biquad circuit with poles located at -450 ± j893.03 and DC gain of 1.3. Make sure the elements in the final circuit are of practically realizable values.

Answer

Tow-Thomas biquad circuit

The Tow-Thomas biquad is a two-integrator-loop circuit using three op-amps: a lossy integrator, an ideal integrator and an inverter in a feedback loop. It gives low-pass and band-pass outputs at the same time, has low sensitivity, and lets ω0\omega_0, QQ and gain be tuned independently.

            R1 (sets Q)
          +--/\/\--+
          |   C1   |
          +---||---+
          |        |
Vin--R4---+--[OA1]-+--> V1 (band-pass)
          ^
          |  V1--R3-->[OA2 integrator, C2]--> V2 (LP)
          |  V2--r--->[OA3 inverter, r/r]---> V3=-V2
          |                                    |
          +------------------R2----------------+

All op-amp (+) inputs are grounded. OA1 is a lossy integrator (R1∥C1R_1 \parallel C_1 in feedback), OA2 an ideal integrator (C2C_2 in feedback), OA3 a unity-gain inverter.

Derivation (ideal op-amps, so each inverting input is a virtual ground):

KCL at the inverting input of OA1:

VinR4+V3R2+V1(1R1+sC1)=0\frac{V_{in}}{R_4} + \frac{V_3}{R_2} + V_1\left(\frac{1}{R_1} + sC_1\right) = 0

OA2 (integrator) and OA3 (inverter):

V2=−V1sR3C2,V3=−V2=V1sR3C2  ⇒  V1=sR3C2V3V_2 = -\frac{V_1}{sR_3C_2}, \qquad V_3 = -V_2 = \frac{V_1}{sR_3C_2} \;\Rightarrow\; V_1 = sR_3C_2V_3

Substituting V1V_1 into the KCL equation:

sR3C2V3(1R1+sC1)+V3R2=−VinR4V3(s2R3C1C2+sR3C2R1+1R2)=−VinR4\begin{aligned} sR_3C_2V_3\left(\frac{1}{R_1} + sC_1\right) + \frac{V_3}{R_2} &= -\frac{V_{in}}{R_4} \\ V_3\left(s^2R_3C_1C_2 + \frac{sR_3C_2}{R_1} + \frac{1}{R_2}\right) &= -\frac{V_{in}}{R_4} \end{aligned}

Dividing by R3C1C2R_3C_1C_2:

V3Vin=−1R3R4C1C2s2+sR1C1+1R2R3C1C2,V2Vin=−V3Vin\frac{V_3}{V_{in}} = \frac{-\dfrac{1}{R_3R_4C_1C_2}}{s^2 + \dfrac{s}{R_1C_1} + \dfrac{1}{R_2R_3C_1C_2}}, \qquad \frac{V_2}{V_{in}} = -\frac{V_3}{V_{in}}

Comparing with T(s)=±Kω02s2+(ω0/Q)s+ω02T(s) = \dfrac{\pm K\omega_0^2}{s^2 + (\omega_0/Q)s + \omega_0^2}:

ω0=1R2R3C1C2,ω0Q=1R1C1,K=R2R4 (dc gain)\omega_0 = \frac{1}{\sqrt{R_2R_3C_1C_2}}, \qquad \frac{\omega_0}{Q} = \frac{1}{R_1C_1}, \qquad K = \frac{R_2}{R_4}\ \text{(dc gain)}

V2V_2 is a non-inverting low-pass output and V3V_3 an inverting one; V1V_1 is a band-pass output.

Design

Step 1: ω0\omega_0 and QQ from the poles. Poles s=−σ±jωds = -\sigma \pm j\omega_d with σ=450\sigma = 450, ωd=893.03\omega_d = 893.03:

ω02=σ2+ωd2=4502+893.032=1,000,002.6  ⇒  ω0≈1000 rad/sω0Q=2σ  ⇒  Q=ω02σ=1000900=1.111\begin{aligned} \omega_0^2 &= \sigma^2 + \omega_d^2 = 450^2 + 893.03^2 = 1{,}000{,}002.6 \;\Rightarrow\; \omega_0 \approx 1000\ \text{rad/s} \\ \frac{\omega_0}{Q} &= 2\sigma \;\Rightarrow\; Q = \frac{\omega_0}{2\sigma} = \frac{1000}{900} = 1.111 \end{aligned}

Required transfer function (dc gain K=1.3K = 1.3):

T(s)=1.3 ω02s2+2σs+ω02=1.3×106s2+900 s+106T(s) = \frac{1.3\,\omega_0^2}{s^2 + 2\sigma s + \omega_0^2} = \frac{1.3 \times 10^{6}}{s^2 + 900\,s + 10^{6}}

Design equations (choose C1=C2=CC_1 = C_2 = C, R2=R3=RR_2 = R_3 = R):

R=1ω0C,R1=QR=Qω0C,R4=R2K,r=any convenient valueR = \frac{1}{\omega_0 C}, \qquad R_1 = QR = \frac{Q}{\omega_0 C}, \qquad R_4 = \frac{R_2}{K}, \qquad r = \text{any convenient value}

Step 2: Element values. Choose C1=C2=C=0.1 μC_1 = C_2 = C = 0.1\ \muF (a standard value that gives resistors in the kΩ\Omega range).

R2=R3=R=1ω0C=11000×0.1×10−6=10 kΩR1=QR=1.111×10 kΩ=11.11 kΩR4=R2K=10 kΩ1.3=7.692 kΩr=10 kΩ (inverter, equal resistors)\begin{aligned} R_2 = R_3 = R &= \frac{1}{\omega_0 C} = \frac{1}{1000 \times 0.1\times10^{-6}} = 10\ \text{k}\Omega \\ R_1 &= QR = 1.111 \times 10\ \text{k}\Omega = 11.11\ \text{k}\Omega \\ R_4 &= \frac{R_2}{K} = \frac{10\ \text{k}\Omega}{1.3} = 7.692\ \text{k}\Omega \\ r &= 10\ \text{k}\Omega \ \text{(inverter, equal resistors)} \end{aligned}

A 1000 rad/s (about 159 Hz) cutoff with Q≈1.1Q \approx 1.1 passes the ECG band and removes higher-frequency noise and interference. Use 1% metal-film resistors (e.g. 7.68 kΩ\Omega for R4R_4, 11.1 kΩ\Omega for R1R_1) and low-noise op-amps.

Final circuit: Tow-Thomas biquad (figure above) with C1=C2=0.1 μFC_1 = C_2 = 0.1\ \mu\text{F}, R1=11.11 kΩR_1 = 11.11\ \text{k}\Omega, R2=R3=10 kΩR_2 = R_3 = 10\ \text{k}\Omega, R4=7.692 kΩR_4 = 7.692\ \text{k}\Omega, r=10 kΩr = 10\ \text{k}\Omega; take the output at V2V_2 (OA2 output) for a positive dc gain of 1.3.

Answer: C=0.1 μFC = 0.1\ \mu\text{F}, R1=11.11 kΩR_1 = 11.11\ \text{k}\Omega, R2=R3=10 kΩR_2 = R_3 = 10\ \text{k}\Omega, R4=7.692 kΩR_4 = 7.692\ \text{k}\Omega, r=10 kΩr = 10\ \text{k}\Omega (all practical values).

  • 2082 Baisakh · 8 marks

Design a filter with poles at -1,000 ± 9949.87j and DC gain of 1.5 using a Tow Thomas Biquad circuit. Your final circuit should have capacitors of value 0.01uF.

Answer

The Tow-Thomas biquad realizes T(s)=Kω02s2+(ω0/Q)s+ω02T(s) = \dfrac{K\omega_0^2}{s^2 + (\omega_0/Q)s + \omega_0^2} with three op-amps (lossy integrator, integrator, inverter).

            R1 (sets Q)
          +--/\/\--+
          |   C1   |
          +---||---+
          |        |
Vin--R4---+--[OA1]-+--> V1 (band-pass)
          ^
          |  V1--R3-->[OA2 integrator, C2]--> V2 (LP)
          |  V2--r--->[OA3 inverter, r/r]---> V3=-V2
          |                                    |
          +------------------R2----------------+

All op-amp (+) inputs are grounded. OA1 is a lossy integrator (R1∥C1R_1 \parallel C_1 in feedback), OA2 an ideal integrator (C2C_2 in feedback), OA3 a unity-gain inverter.

Its low-pass transfer function (output V2V_2) is

V2Vin=1R3R4C1C2s2+sR1C1+1R2R3C1C2,ω0=1R2R3C1C2, ω0Q=1R1C1, K=R2R4\frac{V_2}{V_{in}} = \frac{\dfrac{1}{R_3R_4C_1C_2}}{s^2 + \dfrac{s}{R_1C_1} + \dfrac{1}{R_2R_3C_1C_2}}, \quad \omega_0 = \frac{1}{\sqrt{R_2R_3C_1C_2}},\ \frac{\omega_0}{Q} = \frac{1}{R_1C_1},\ K = \frac{R_2}{R_4}

Design

Step 1: ω0\omega_0 and QQ from the poles. Poles s=−σ±jωds = -\sigma \pm j\omega_d with σ=1000\sigma = 1000, ωd=9949.87\omega_d = 9949.87:

ω02=σ2+ωd2=10002+9949.872=99,999,913≈108  ⇒  ω0≈10,000 rad/sω0Q=2σ  ⇒  Q=ω02σ=100002000=5\begin{aligned} \omega_0^2 &= \sigma^2 + \omega_d^2 = 1000^2 + 9949.87^2 = 99{,}999{,}913 \approx 10^8 \;\Rightarrow\; \omega_0 \approx 10{,}000\ \text{rad/s} \\ \frac{\omega_0}{Q} &= 2\sigma \;\Rightarrow\; Q = \frac{\omega_0}{2\sigma} = \frac{10000}{2000} = 5 \end{aligned}

Required transfer function (dc gain K=1.5K = 1.5):

T(s)=1.5 ω02s2+2σs+ω02=1.5×108s2+2000 s+108T(s) = \frac{1.5\,\omega_0^2}{s^2 + 2\sigma s + \omega_0^2} = \frac{1.5 \times 10^{8}}{s^2 + 2000\,s + 10^{8}}

Design equations (choose C1=C2=CC_1 = C_2 = C, R2=R3=RR_2 = R_3 = R):

R=1ω0C,R1=QR=Qω0C,R4=R2K,r=any convenient valueR = \frac{1}{\omega_0 C}, \qquad R_1 = QR = \frac{Q}{\omega_0 C}, \qquad R_4 = \frac{R_2}{K}, \qquad r = \text{any convenient value}

Step 2: Element values. Given C1=C2=C=0.01 μC_1 = C_2 = C = 0.01\ \muF.

R2=R3=R=1ω0C=110,000×0.01×10−6=10 kΩR1=QR=5×10 kΩ=50 kΩR4=R2K=10 kΩ1.5=6.667 kΩr=10 kΩ (inverter, equal resistors)\begin{aligned} R_2 = R_3 = R &= \frac{1}{\omega_0 C} = \frac{1}{10{,}000 \times 0.01\times10^{-6}} = 10\ \text{k}\Omega \\ R_1 &= QR = 5 \times 10\ \text{k}\Omega = 50\ \text{k}\Omega \\ R_4 &= \frac{R_2}{K} = \frac{10\ \text{k}\Omega}{1.5} = 6.667\ \text{k}\Omega \\ r &= 10\ \text{k}\Omega \ \text{(inverter, equal resistors)} \end{aligned}

Final circuit: Tow-Thomas biquad (figure above) with C1=C2=0.01 μFC_1 = C_2 = 0.01\ \mu\text{F}, R1=50 kΩR_1 = 50\ \text{k}\Omega, R2=R3=10 kΩR_2 = R_3 = 10\ \text{k}\Omega, R4=6.667 kΩR_4 = 6.667\ \text{k}\Omega, r=10 kΩr = 10\ \text{k}\Omega; take the output at V2V_2 (OA2 output) for a positive dc gain of 1.5.

Answer: C=0.01 μFC = 0.01\ \mu\text{F}, R1=50 kΩR_1 = 50\ \text{k}\Omega, R2=R3=10 kΩR_2 = R_3 = 10\ \text{k}\Omega, R4=6.667 kΩR_4 = 6.667\ \text{k}\Omega, r=10 kΩr = 10\ \text{k}\Omega (all practical values).

  • 2080 Baisakh · 6 marks

Design a second order low pass filter with poles at -10000 ± j17320.51 and Dc Gain of 2.5 using a Tow Thomas Biquad Circuit. Your final circuit should have capacitors of value 0.001uF.

Answer

The Tow-Thomas biquad realizes T(s)=Kω02s2+(ω0/Q)s+ω02T(s) = \dfrac{K\omega_0^2}{s^2 + (\omega_0/Q)s + \omega_0^2} with three op-amps (lossy integrator, integrator, inverter).

            R1 (sets Q)
          +--/\/\--+
          |   C1   |
          +---||---+
          |        |
Vin--R4---+--[OA1]-+--> V1 (band-pass)
          ^
          |  V1--R3-->[OA2 integrator, C2]--> V2 (LP)
          |  V2--r--->[OA3 inverter, r/r]---> V3=-V2
          |                                    |
          +------------------R2----------------+

All op-amp (+) inputs are grounded. OA1 is a lossy integrator (R1∥C1R_1 \parallel C_1 in feedback), OA2 an ideal integrator (C2C_2 in feedback), OA3 a unity-gain inverter.

Low-pass transfer function (output V2V_2):

V2Vin=1R3R4C1C2s2+sR1C1+1R2R3C1C2,ω0=1R2R3C1C2, ω0Q=1R1C1, K=R2R4\frac{V_2}{V_{in}} = \frac{\dfrac{1}{R_3R_4C_1C_2}}{s^2 + \dfrac{s}{R_1C_1} + \dfrac{1}{R_2R_3C_1C_2}}, \quad \omega_0 = \frac{1}{\sqrt{R_2R_3C_1C_2}},\ \frac{\omega_0}{Q} = \frac{1}{R_1C_1},\ K = \frac{R_2}{R_4}

Design

Step 1: ω0\omega_0 and QQ from the poles. Poles s=−σ±jωds = -\sigma \pm j\omega_d with σ=10000\sigma = 10000, ωd=17320.51\omega_d = 17320.51:

ω02=σ2+ωd2=100002+17320.512=400,000,067≈4×108  ⇒  ω0≈20,000 rad/sω0Q=2σ  ⇒  Q=ω02σ=2000020000=1\begin{aligned} \omega_0^2 &= \sigma^2 + \omega_d^2 = 10000^2 + 17320.51^2 = 400{,}000{,}067 \approx 4\times10^8 \;\Rightarrow\; \omega_0 \approx 20{,}000\ \text{rad/s} \\ \frac{\omega_0}{Q} &= 2\sigma \;\Rightarrow\; Q = \frac{\omega_0}{2\sigma} = \frac{20000}{20000} = 1 \end{aligned}

Required transfer function (dc gain K=2.5K = 2.5):

T(s)=2.5 ω02s2+2σs+ω02=2.5×4×108s2+20000 s+4×108T(s) = \frac{2.5\,\omega_0^2}{s^2 + 2\sigma s + \omega_0^2} = \frac{2.5 \times 4\times10^{8}}{s^2 + 20000\,s + 4\times10^{8}}

Design equations (choose C1=C2=CC_1 = C_2 = C, R2=R3=RR_2 = R_3 = R):

R=1ω0C,R1=QR=Qω0C,R4=R2K,r=any convenient valueR = \frac{1}{\omega_0 C}, \qquad R_1 = QR = \frac{Q}{\omega_0 C}, \qquad R_4 = \frac{R_2}{K}, \qquad r = \text{any convenient value}

Step 2: Element values. Given C1=C2=C=0.001 μC_1 = C_2 = C = 0.001\ \muF.

R2=R3=R=1ω0C=120,000×0.001×10−6=50 kΩR1=QR=1×50 kΩ=50 kΩR4=R2K=50 kΩ2.5=20 kΩr=10 kΩ (inverter, equal resistors)\begin{aligned} R_2 = R_3 = R &= \frac{1}{\omega_0 C} = \frac{1}{20{,}000 \times 0.001\times10^{-6}} = 50\ \text{k}\Omega \\ R_1 &= QR = 1 \times 50\ \text{k}\Omega = 50\ \text{k}\Omega \\ R_4 &= \frac{R_2}{K} = \frac{50\ \text{k}\Omega}{2.5} = 20\ \text{k}\Omega \\ r &= 10\ \text{k}\Omega \ \text{(inverter, equal resistors)} \end{aligned}

Final circuit: Tow-Thomas biquad (figure above) with C1=C2=0.001 μFC_1 = C_2 = 0.001\ \mu\text{F}, R1=50 kΩR_1 = 50\ \text{k}\Omega, R2=R3=50 kΩR_2 = R_3 = 50\ \text{k}\Omega, R4=20 kΩR_4 = 20\ \text{k}\Omega, r=10 kΩr = 10\ \text{k}\Omega; take the output at V2V_2 (OA2 output) for a positive dc gain of 2.5.

Answer: C=0.001 μFC = 0.001\ \mu\text{F}, R1=50 kΩR_1 = 50\ \text{k}\Omega, R2=R3=50 kΩR_2 = R_3 = 50\ \text{k}\Omega, R4=20 kΩR_4 = 20\ \text{k}\Omega, r=10 kΩr = 10\ \text{k}\Omega (all practical values).

  • 2079 Bhadra · 3+5 marks

What is Quality factor and center frequency of low pass biquad filter? Explain with suitable diagram. Realize following low pass filter transfer function using Tow Thomas biquad circuit. T(s) = -2000/(s² + 500s + 1000000)

Answer

Quality factor and centre frequency of a low-pass biquad

A second-order low-pass biquad has

T(s)=Kω02s2+ω0Qs+ω02T(s) = \frac{K\omega_0^2}{s^2 + \dfrac{\omega_0}{Q}s + \omega_0^2}
  • Centre (pole / natural) frequency ω0\omega_0: the magnitude of the poles, ω0=∣p∣=σ2+ωd2\omega_0 = |p| = \sqrt{\sigma^2 + \omega_d^2}. It sets where the response turns over; at ω=ω0\omega = \omega_0 the phase is −90∘-90^\circ.
  • Quality factor QQ: Q=ω02σQ = \dfrac{\omega_0}{2\sigma}, where σ\sigma is the distance of the poles from the jωj\omega axis. It measures how sharp the response is near ω0\omega_0: ∣T(jω0)∣=KQ|T(j\omega_0)| = KQ. A large QQ puts the poles close to the jωj\omega axis and gives a high peak; Q=0.707Q = 0.707 gives the maximally flat (Butterworth) shape; Q<0.5Q < 0.5 gives real poles.
 |T|
  |        Q = 5 (sharp peak)
  |        /\
  |       /  \
 K|------/-.--\--- Q = 0.707 (flat)
  |       '. \ \
  |          '.\ \
  |             '-\----
  +-----------+--------> w
              w0

The pole angle from the negative real axis is ψ=cos⁡−1 ⁣(1/2Q)\psi = \cos^{-1}\!\big(1/2Q\big), so higher QQ means poles closer to the jωj\omega axis.

Tow-Thomas circuit used

            R1 (sets Q)
          +--/\/\--+
          |   C1   |
          +---||---+
          |        |
Vin--R4---+--[OA1]-+--> V1 (band-pass)
          ^
          |  V1--R3-->[OA2 integrator, C2]--> V2 (LP)
          |  V2--r--->[OA3 inverter, r/r]---> V3=-V2
          |                                    |
          +------------------R2----------------+

All op-amp (+) inputs are grounded. OA1 is a lossy integrator (R1∥C1R_1 \parallel C_1 in feedback), OA2 an ideal integrator (C2C_2 in feedback), OA3 a unity-gain inverter.

Its inverting low-pass output is

V3Vin=−1R3R4C1C2s2+sR1C1+1R2R3C1C2\frac{V_3}{V_{in}} = \frac{-\dfrac{1}{R_3R_4C_1C_2}}{s^2 + \dfrac{s}{R_1C_1} + \dfrac{1}{R_2R_3C_1C_2}}

with ω0=1/R2R3C1C2\omega_0 = 1/\sqrt{R_2R_3C_1C_2}, ω0/Q=1/(R1C1)\omega_0/Q = 1/(R_1C_1), K=R2/R4K = R_2/R_4. With C1=C2=CC_1 = C_2 = C, R2=R3=RR_2 = R_3 = R: R=1/(ω0C)R = 1/(\omega_0C), R1=QRR_1 = QR, R4=R/KR_4 = R/K.

Realization of T(s)=−2000s2+500s+1,000,000T(s) = \dfrac{-2000}{s^2 + 500s + 1{,}000{,}000}

Step 1: Parameters.

ω02=106  ⇒  ω0=1000 rad/sω0Q=500  ⇒  Q=1000500=2dc gain=T(0)=−2000106=−0.002,so K=R2R4=0.002\begin{aligned} \omega_0^2 &= 10^6 \;\Rightarrow\; \omega_0 = 1000\ \text{rad/s} \\ \frac{\omega_0}{Q} &= 500 \;\Rightarrow\; Q = \frac{1000}{500} = 2 \\ \text{dc gain} &= T(0) = \frac{-2000}{10^6} = -0.002, \quad \text{so } K = \frac{R_2}{R_4} = 0.002 \end{aligned}

The gain is negative, so the output is taken at V3V_3 (the inverter output), which gives −1/(R3R4C1C2)s2+s/(R1C1)+1/(R2R3C1C2)-\dfrac{1/(R_3R_4C_1C_2)}{s^2 + s/(R_1C_1) + 1/(R_2R_3C_1C_2)}.

Step 2: Element values. Choose C1=C2=C=1 μC_1 = C_2 = C = 1\ \muF, R2=R3=RR_2 = R_3 = R (with C=0.1 μC = 0.1\ \muF, R4R_4 would be 5 MΩ\Omega, which is too large, so 1 μ1\ \muF is chosen).

R2=R3=R=1ω0C=11000×10−6=1 kΩR1=QR=2×1=2 kΩR4=R2K=1 kΩ0.002=500 kΩr=10 kΩ (inverter)\begin{aligned} R_2 = R_3 = R &= \frac{1}{\omega_0 C} = \frac{1}{1000 \times 10^{-6}} = 1\ \text{k}\Omega \\ R_1 &= QR = 2 \times 1 = 2\ \text{k}\Omega \\ R_4 &= \frac{R_2}{K} = \frac{1\ \text{k}\Omega}{0.002} = 500\ \text{k}\Omega \\ r &= 10\ \text{k}\Omega \ \text{(inverter)} \end{aligned}

Check: numerator 1R3R4C1C2=1103×5×105×10−12=2000\dfrac{1}{R_3R_4C_1C_2} = \dfrac{1}{10^3 \times 5\times10^5 \times 10^{-12}} = 2000; 1R1C1=12000×10−6=500\dfrac{1}{R_1C_1} = \dfrac{1}{2000\times10^{-6}} = 500; 1R2R3C2=106\dfrac{1}{R_2R_3C^2} = 10^6. All coefficients match.

Answer: C1=C2=1 μC_1 = C_2 = 1\ \muF, R1=2R_1 = 2 kΩ\Omega, R2=R3=1R_2 = R_3 = 1 kΩ\Omega, R4=500R_4 = 500 kΩ\Omega, r=10r = 10 kΩ\Omega, output at V3V_3 (OA3).

  • 2073 Shrawan · 4+4 marks

Draw the circuit diagram of Tow Thomas low pass filter and derive its transfer function. Realize following low pass filter using Tow Thomas biquad circuit. T(s) = -2000/(s² + 500s + 1000000)

Answer

Tow-Thomas low-pass biquad

The Tow-Thomas biquad is a two-integrator-loop circuit using three op-amps: a lossy integrator, an ideal integrator and an inverter in a feedback loop. It gives low-pass and band-pass outputs at the same time, has low sensitivity, and lets ω0\omega_0, QQ and gain be tuned independently.

            R1 (sets Q)
          +--/\/\--+
          |   C1   |
          +---||---+
          |        |
Vin--R4---+--[OA1]-+--> V1 (band-pass)
          ^
          |  V1--R3-->[OA2 integrator, C2]--> V2 (LP)
          |  V2--r--->[OA3 inverter, r/r]---> V3=-V2
          |                                    |
          +------------------R2----------------+

All op-amp (+) inputs are grounded. OA1 is a lossy integrator (R1∥C1R_1 \parallel C_1 in feedback), OA2 an ideal integrator (C2C_2 in feedback), OA3 a unity-gain inverter.

Derivation (ideal op-amps, so each inverting input is a virtual ground):

KCL at the inverting input of OA1:

VinR4+V3R2+V1(1R1+sC1)=0\frac{V_{in}}{R_4} + \frac{V_3}{R_2} + V_1\left(\frac{1}{R_1} + sC_1\right) = 0

OA2 (integrator) and OA3 (inverter):

V2=−V1sR3C2,V3=−V2=V1sR3C2  ⇒  V1=sR3C2V3V_2 = -\frac{V_1}{sR_3C_2}, \qquad V_3 = -V_2 = \frac{V_1}{sR_3C_2} \;\Rightarrow\; V_1 = sR_3C_2V_3

Substituting V1V_1 into the KCL equation:

sR3C2V3(1R1+sC1)+V3R2=−VinR4V3(s2R3C1C2+sR3C2R1+1R2)=−VinR4\begin{aligned} sR_3C_2V_3\left(\frac{1}{R_1} + sC_1\right) + \frac{V_3}{R_2} &= -\frac{V_{in}}{R_4} \\ V_3\left(s^2R_3C_1C_2 + \frac{sR_3C_2}{R_1} + \frac{1}{R_2}\right) &= -\frac{V_{in}}{R_4} \end{aligned}

Dividing by R3C1C2R_3C_1C_2:

V3Vin=−1R3R4C1C2s2+sR1C1+1R2R3C1C2,V2Vin=−V3Vin\frac{V_3}{V_{in}} = \frac{-\dfrac{1}{R_3R_4C_1C_2}}{s^2 + \dfrac{s}{R_1C_1} + \dfrac{1}{R_2R_3C_1C_2}}, \qquad \frac{V_2}{V_{in}} = -\frac{V_3}{V_{in}}

Comparing with T(s)=±Kω02s2+(ω0/Q)s+ω02T(s) = \dfrac{\pm K\omega_0^2}{s^2 + (\omega_0/Q)s + \omega_0^2}:

ω0=1R2R3C1C2,ω0Q=1R1C1,K=R2R4 (dc gain)\omega_0 = \frac{1}{\sqrt{R_2R_3C_1C_2}}, \qquad \frac{\omega_0}{Q} = \frac{1}{R_1C_1}, \qquad K = \frac{R_2}{R_4}\ \text{(dc gain)}

V2V_2 is a non-inverting low-pass output and V3V_3 an inverting one; V1V_1 is a band-pass output.

Design equations (choose C1=C2=CC_1 = C_2 = C, R2=R3=RR_2 = R_3 = R):

R=1ω0C,R1=QR=Qω0C,R4=R2K,r=any convenient valueR = \frac{1}{\omega_0 C}, \qquad R_1 = QR = \frac{Q}{\omega_0 C}, \qquad R_4 = \frac{R_2}{K}, \qquad r = \text{any convenient value}

Realization of T(s)=−2000s2+500s+1,000,000T(s) = \dfrac{-2000}{s^2 + 500s + 1{,}000{,}000}

Step 1: Parameters.

ω02=106  ⇒  ω0=1000 rad/sω0Q=500  ⇒  Q=1000500=2dc gain=T(0)=−2000106=−0.002,so K=R2R4=0.002\begin{aligned} \omega_0^2 &= 10^6 \;\Rightarrow\; \omega_0 = 1000\ \text{rad/s} \\ \frac{\omega_0}{Q} &= 500 \;\Rightarrow\; Q = \frac{1000}{500} = 2 \\ \text{dc gain} &= T(0) = \frac{-2000}{10^6} = -0.002, \quad \text{so } K = \frac{R_2}{R_4} = 0.002 \end{aligned}

The gain is negative, so the output is taken at V3V_3 (the inverter output), which gives −1/(R3R4C1C2)s2+s/(R1C1)+1/(R2R3C1C2)-\dfrac{1/(R_3R_4C_1C_2)}{s^2 + s/(R_1C_1) + 1/(R_2R_3C_1C_2)}.

Step 2: Element values. Choose C1=C2=C=1 μC_1 = C_2 = C = 1\ \muF, R2=R3=RR_2 = R_3 = R (with C=0.1 μC = 0.1\ \muF, R4R_4 would be 5 MΩ\Omega, which is too large, so 1 μ1\ \muF is chosen).

R2=R3=R=1ω0C=11000×10−6=1 kΩR1=QR=2×1=2 kΩR4=R2K=1 kΩ0.002=500 kΩr=10 kΩ (inverter)\begin{aligned} R_2 = R_3 = R &= \frac{1}{\omega_0 C} = \frac{1}{1000 \times 10^{-6}} = 1\ \text{k}\Omega \\ R_1 &= QR = 2 \times 1 = 2\ \text{k}\Omega \\ R_4 &= \frac{R_2}{K} = \frac{1\ \text{k}\Omega}{0.002} = 500\ \text{k}\Omega \\ r &= 10\ \text{k}\Omega \ \text{(inverter)} \end{aligned}

Check: numerator 1R3R4C1C2=1103×5×105×10−12=2000\dfrac{1}{R_3R_4C_1C_2} = \dfrac{1}{10^3 \times 5\times10^5 \times 10^{-12}} = 2000; 1R1C1=12000×10−6=500\dfrac{1}{R_1C_1} = \dfrac{1}{2000\times10^{-6}} = 500; 1R2R3C2=106\dfrac{1}{R_2R_3C^2} = 10^6. All coefficients match.

Answer: C1=C2=1 μC_1 = C_2 = 1\ \muF, R1=2R_1 = 2 kΩ\Omega, R2=R3=1R_2 = R_3 = 1 kΩ\Omega, R4=500R_4 = 500 kΩ\Omega, r=10r = 10 kΩ\Omega, output at V3V_3 (OA3).

  • 2078 Bhadra · 5+4 marks

Derive the transfer function of Tow-Thomas band pass biquad and design it with centre frequency of 1000 rad/sec, bandwidth of 200 rad/sec and a maximum gain of 1.

Answer

Tow-Thomas band-pass biquad

The band-pass output of the Tow-Thomas biquad is taken at the output of the lossy integrator OA1.

            R1 (sets Q)
          +--/\/\--+
          |   C1   |
          +---||---+
          |        |
Vin--R4---+--[OA1]-+--> V1 (band-pass)
          ^
          |  V1--R3-->[OA2 integrator, C2]--> V2 (LP)
          |  V2--r--->[OA3 inverter, r/r]---> V3=-V2
          |                                    |
          +------------------R2----------------+

All op-amp (+) inputs are grounded. OA1 is a lossy integrator (R1∥C1R_1 \parallel C_1 in feedback), OA2 an ideal integrator (C2C_2 in feedback), OA3 a unity-gain inverter.

Derivation. KCL at the inverting input of OA1 (virtual ground):

VinR4+V3R2+V1(1R1+sC1)=0\frac{V_{in}}{R_4} + \frac{V_3}{R_2} + V_1\left(\frac{1}{R_1} + sC_1\right) = 0

OA2 integrates and OA3 inverts:

V2=−V1sR3C2,V3=−V2=V1sR3C2V_2 = -\frac{V_1}{sR_3C_2}, \qquad V_3 = -V_2 = \frac{V_1}{sR_3C_2}

Substituting V3V_3:

V1(sC1+1R1+1sR2R3C2)=−VinR4V_1\left(sC_1 + \frac{1}{R_1} + \frac{1}{sR_2R_3C_2}\right) = -\frac{V_{in}}{R_4}

Multiplying both sides by s/C1s/C_1:

V1Vin=−sR4C1s2+sR1C1+1R2R3C1C2\frac{V_1}{V_{in}} = \frac{-\dfrac{s}{R_4C_1}}{s^2 + \dfrac{s}{R_1C_1} + \dfrac{1}{R_2R_3C_1C_2}}

Comparing with the standard band-pass form T(s)=−H(ω0/Q)ss2+(ω0/Q)s+ω02T(s) = \dfrac{-H(\omega_0/Q)s}{s^2 + (\omega_0/Q)s + \omega_0^2}:

ω0=1R2R3C1C2,BW=ω0Q=1R1C1,Q=ω0R1C1\omega_0 = \frac{1}{\sqrt{R_2R_3C_1C_2}}, \qquad \text{BW} = \frac{\omega_0}{Q} = \frac{1}{R_1C_1}, \qquad Q = \omega_0R_1C_1

and the gain at the centre frequency s=jω0s = j\omega_0 is

∣T(jω0)∣=1/(R4C1)1/(R1C1)=R1R4|T(j\omega_0)| = \frac{1/(R_4C_1)}{1/(R_1C_1)} = \frac{R_1}{R_4}

So ω0\omega_0 is set by R2,R3R_2, R_3, the bandwidth by R1R_1 and the peak gain by R4R_4, independently.

Design: ω0=1000\omega_0 = 1000 rad/s, BW = 200 rad/s, maximum gain 1

Step 1: Parameters.

Q=ω0BW=1000200=5,H=R1R4=1Q = \frac{\omega_0}{\text{BW}} = \frac{1000}{200} = 5, \qquad H = \frac{R_1}{R_4} = 1

Required: T(s)=−200ss2+200s+106T(s) = \dfrac{-200s}{s^2 + 200s + 10^6}.

Step 2: Element values. Choose C1=C2=C=0.1 μC_1 = C_2 = C = 0.1\ \muF and R2=R3=RR_2 = R_3 = R.

R2=R3=R=1ω0C=11000×0.1×10−6=10 kΩR1=1BW⋅C=Qω0C=5×10=50 kΩR4=R1H=50 kΩr=10 kΩ (inverter)\begin{aligned} R_2 = R_3 = R &= \frac{1}{\omega_0 C} = \frac{1}{1000 \times 0.1\times10^{-6}} = 10\ \text{k}\Omega \\ R_1 &= \frac{1}{\text{BW}\cdot C} = \frac{Q}{\omega_0 C} = 5 \times 10 = 50\ \text{k}\Omega \\ R_4 &= \frac{R_1}{H} = 50\ \text{k}\Omega \\ r &= 10\ \text{k}\Omega\ \text{(inverter)} \end{aligned}

Check: 1/(R1C)=1/(5×104×10−7)=2001/(R_1C) = 1/(5\times10^4 \times 10^{-7}) = 200 rad/s (bandwidth), 1/(R2C2)=1/(104×10−7)2=1061/(R^2C^2) = 1/(10^4\times10^{-7})^2 = 10^6, and 1/(R4C)=2001/(R_4C) = 200, so T(s)=−200s/(s2+200s+106)T(s) = -200s/(s^2+200s+10^6) with ∣T(j1000)∣=1|T(j1000)| = 1.

Answer: C1=C2=0.1 μC_1 = C_2 = 0.1\ \muF, R1=R4=50R_1 = R_4 = 50 kΩ\Omega, R2=R3=10R_2 = R_3 = 10 kΩ\Omega, r=10r = 10 kΩ\Omega; output at V1V_1 (OA1).

  • 2082 Bhadra · 5 marks

Draw a neat circuit diagram of Tow-Thomas band-pass biquad and derive its transfer function.

Answer

Tow-Thomas band-pass biquad

The band-pass output of the Tow-Thomas biquad is taken at the output of the lossy integrator OA1.

            R1 (sets Q)
          +--/\/\--+
          |   C1   |
          +---||---+
          |        |
Vin--R4---+--[OA1]-+--> V1 (band-pass)
          ^
          |  V1--R3-->[OA2 integrator, C2]--> V2 (LP)
          |  V2--r--->[OA3 inverter, r/r]---> V3=-V2
          |                                    |
          +------------------R2----------------+

All op-amp (+) inputs are grounded. OA1 is a lossy integrator (R1∥C1R_1 \parallel C_1 in feedback), OA2 an ideal integrator (C2C_2 in feedback), OA3 a unity-gain inverter.

Derivation. KCL at the inverting input of OA1 (virtual ground):

VinR4+V3R2+V1(1R1+sC1)=0\frac{V_{in}}{R_4} + \frac{V_3}{R_2} + V_1\left(\frac{1}{R_1} + sC_1\right) = 0

OA2 integrates and OA3 inverts:

V2=−V1sR3C2,V3=−V2=V1sR3C2V_2 = -\frac{V_1}{sR_3C_2}, \qquad V_3 = -V_2 = \frac{V_1}{sR_3C_2}

Substituting V3V_3:

V1(sC1+1R1+1sR2R3C2)=−VinR4V_1\left(sC_1 + \frac{1}{R_1} + \frac{1}{sR_2R_3C_2}\right) = -\frac{V_{in}}{R_4}

Multiplying both sides by s/C1s/C_1:

V1Vin=−sR4C1s2+sR1C1+1R2R3C1C2\frac{V_1}{V_{in}} = \frac{-\dfrac{s}{R_4C_1}}{s^2 + \dfrac{s}{R_1C_1} + \dfrac{1}{R_2R_3C_1C_2}}

Comparing with the standard band-pass form T(s)=−H(ω0/Q)ss2+(ω0/Q)s+ω02T(s) = \dfrac{-H(\omega_0/Q)s}{s^2 + (\omega_0/Q)s + \omega_0^2}:

ω0=1R2R3C1C2,BW=ω0Q=1R1C1,Q=ω0R1C1\omega_0 = \frac{1}{\sqrt{R_2R_3C_1C_2}}, \qquad \text{BW} = \frac{\omega_0}{Q} = \frac{1}{R_1C_1}, \qquad Q = \omega_0R_1C_1

and the gain at the centre frequency s=jω0s = j\omega_0 is

∣T(jω0)∣=1/(R4C1)1/(R1C1)=R1R4|T(j\omega_0)| = \frac{1/(R_4C_1)}{1/(R_1C_1)} = \frac{R_1}{R_4}

So ω0\omega_0 is set by R2,R3R_2, R_3, the bandwidth by R1R_1 and the peak gain by R4R_4, independently.

  • 2071 Chaitra · 9 marks

Draw a neat and clean circuit diagram of Tow-Thomas Low Pass Biquad filter and derive it's transfer function. Design a low pass filter using Tow-Thomas Biquad circuit which has poles at 1000 ± 8994.03j [as printed] and DC gain of 1.89. Use 0.01μF capacitor in your design.

Answer

Tow-Thomas low-pass biquad

The Tow-Thomas biquad is a two-integrator-loop circuit using three op-amps: a lossy integrator, an ideal integrator and an inverter in a feedback loop. It gives low-pass and band-pass outputs at the same time, has low sensitivity, and lets ω0\omega_0, QQ and gain be tuned independently.

            R1 (sets Q)
          +--/\/\--+
          |   C1   |
          +---||---+
          |        |
Vin--R4---+--[OA1]-+--> V1 (band-pass)
          ^
          |  V1--R3-->[OA2 integrator, C2]--> V2 (LP)
          |  V2--r--->[OA3 inverter, r/r]---> V3=-V2
          |                                    |
          +------------------R2----------------+

All op-amp (+) inputs are grounded. OA1 is a lossy integrator (R1∥C1R_1 \parallel C_1 in feedback), OA2 an ideal integrator (C2C_2 in feedback), OA3 a unity-gain inverter.

Derivation (ideal op-amps, so each inverting input is a virtual ground):

KCL at the inverting input of OA1:

VinR4+V3R2+V1(1R1+sC1)=0\frac{V_{in}}{R_4} + \frac{V_3}{R_2} + V_1\left(\frac{1}{R_1} + sC_1\right) = 0

OA2 (integrator) and OA3 (inverter):

V2=−V1sR3C2,V3=−V2=V1sR3C2  ⇒  V1=sR3C2V3V_2 = -\frac{V_1}{sR_3C_2}, \qquad V_3 = -V_2 = \frac{V_1}{sR_3C_2} \;\Rightarrow\; V_1 = sR_3C_2V_3

Substituting V1V_1 into the KCL equation:

sR3C2V3(1R1+sC1)+V3R2=−VinR4V3(s2R3C1C2+sR3C2R1+1R2)=−VinR4\begin{aligned} sR_3C_2V_3\left(\frac{1}{R_1} + sC_1\right) + \frac{V_3}{R_2} &= -\frac{V_{in}}{R_4} \\ V_3\left(s^2R_3C_1C_2 + \frac{sR_3C_2}{R_1} + \frac{1}{R_2}\right) &= -\frac{V_{in}}{R_4} \end{aligned}

Dividing by R3C1C2R_3C_1C_2:

V3Vin=−1R3R4C1C2s2+sR1C1+1R2R3C1C2,V2Vin=−V3Vin\frac{V_3}{V_{in}} = \frac{-\dfrac{1}{R_3R_4C_1C_2}}{s^2 + \dfrac{s}{R_1C_1} + \dfrac{1}{R_2R_3C_1C_2}}, \qquad \frac{V_2}{V_{in}} = -\frac{V_3}{V_{in}}

Comparing with T(s)=±Kω02s2+(ω0/Q)s+ω02T(s) = \dfrac{\pm K\omega_0^2}{s^2 + (\omega_0/Q)s + \omega_0^2}:

ω0=1R2R3C1C2,ω0Q=1R1C1,K=R2R4 (dc gain)\omega_0 = \frac{1}{\sqrt{R_2R_3C_1C_2}}, \qquad \frac{\omega_0}{Q} = \frac{1}{R_1C_1}, \qquad K = \frac{R_2}{R_4}\ \text{(dc gain)}

V2V_2 is a non-inverting low-pass output and V3V_3 an inverting one; V1V_1 is a band-pass output.

Design

Step 1: ω0\omega_0 and QQ from the poles. Poles s=−σ±jωds = -\sigma \pm j\omega_d with σ=1000\sigma = 1000, ωd=8994.03\omega_d = 8994.03:

ω02=σ2+ωd2=10002+8994.032=81,892,576  ⇒  ω0≈9049.45 rad/sω0Q=2σ  ⇒  Q=ω02σ=9049.452000=4.525\begin{aligned} \omega_0^2 &= \sigma^2 + \omega_d^2 = 1000^2 + 8994.03^2 = 81{,}892{,}576 \;\Rightarrow\; \omega_0 \approx 9049.45\ \text{rad/s} \\ \frac{\omega_0}{Q} &= 2\sigma \;\Rightarrow\; Q = \frac{\omega_0}{2\sigma} = \frac{9049.45}{2000} = 4.525 \end{aligned}

Required transfer function (dc gain K=1.89K = 1.89):

T(s)=1.89 ω02s2+2σs+ω02=1.89×8.189×107s2+2000 s+8.189×107T(s) = \frac{1.89\,\omega_0^2}{s^2 + 2\sigma s + \omega_0^2} = \frac{1.89 \times 8.189\times10^{7}}{s^2 + 2000\,s + 8.189\times10^{7}}

Design equations (choose C1=C2=CC_1 = C_2 = C, R2=R3=RR_2 = R_3 = R):

R=1ω0C,R1=QR=Qω0C,R4=R2K,r=any convenient valueR = \frac{1}{\omega_0 C}, \qquad R_1 = QR = \frac{Q}{\omega_0 C}, \qquad R_4 = \frac{R_2}{K}, \qquad r = \text{any convenient value}

Step 2: Element values. Given C1=C2=C=0.01 μC_1 = C_2 = C = 0.01\ \muF. (The poles are printed as 1000±j8994.031000 \pm j8994.03; a stable filter needs left-half-plane poles, so −1000±j8994.03-1000 \pm j8994.03 is used.)

R2=R3=R=1ω0C=19049.45×0.01×10−6=11.05 kΩR1=QR=4.525×11.05 kΩ=50 kΩR4=R2K=11.05 kΩ1.89=5.847 kΩr=10 kΩ (inverter, equal resistors)\begin{aligned} R_2 = R_3 = R &= \frac{1}{\omega_0 C} = \frac{1}{9049.45 \times 0.01\times10^{-6}} = 11.05\ \text{k}\Omega \\ R_1 &= QR = 4.525 \times 11.05\ \text{k}\Omega = 50\ \text{k}\Omega \\ R_4 &= \frac{R_2}{K} = \frac{11.05\ \text{k}\Omega}{1.89} = 5.847\ \text{k}\Omega \\ r &= 10\ \text{k}\Omega \ \text{(inverter, equal resistors)} \end{aligned}

Final circuit: Tow-Thomas biquad (figure above) with C1=C2=0.01 μFC_1 = C_2 = 0.01\ \mu\text{F}, R1=50 kΩR_1 = 50\ \text{k}\Omega, R2=R3=11.05 kΩR_2 = R_3 = 11.05\ \text{k}\Omega, R4=5.847 kΩR_4 = 5.847\ \text{k}\Omega, r=10 kΩr = 10\ \text{k}\Omega; take the output at V2V_2 (OA2 output) for a positive dc gain of 1.89.

Answer: C=0.01 μFC = 0.01\ \mu\text{F}, R1=50 kΩR_1 = 50\ \text{k}\Omega, R2=R3=11.05 kΩR_2 = R_3 = 11.05\ \text{k}\Omega, R4=5.847 kΩR_4 = 5.847\ \text{k}\Omega, r=10 kΩr = 10\ \text{k}\Omega (all practical values).

  • 2071 Shrawan · 4+4 marks

Draw the circuit diagram of Tow Thomas biquad filter and derive its lowpass transfer function. Design a second order Butterworth lowpass filter having half power frequency of 5 kHz using Tow Thomas biquad circuit. Your final circuit should have all capacitors of 0.001μF.

Answer

Tow-Thomas low-pass biquad

The Tow-Thomas biquad is a two-integrator-loop circuit using three op-amps: a lossy integrator, an ideal integrator and an inverter in a feedback loop. It gives low-pass and band-pass outputs at the same time, has low sensitivity, and lets ω0\omega_0, QQ and gain be tuned independently.

            R1 (sets Q)
          +--/\/\--+
          |   C1   |
          +---||---+
          |        |
Vin--R4---+--[OA1]-+--> V1 (band-pass)
          ^
          |  V1--R3-->[OA2 integrator, C2]--> V2 (LP)
          |  V2--r--->[OA3 inverter, r/r]---> V3=-V2
          |                                    |
          +------------------R2----------------+

All op-amp (+) inputs are grounded. OA1 is a lossy integrator (R1∥C1R_1 \parallel C_1 in feedback), OA2 an ideal integrator (C2C_2 in feedback), OA3 a unity-gain inverter.

Derivation (ideal op-amps, so each inverting input is a virtual ground):

KCL at the inverting input of OA1:

VinR4+V3R2+V1(1R1+sC1)=0\frac{V_{in}}{R_4} + \frac{V_3}{R_2} + V_1\left(\frac{1}{R_1} + sC_1\right) = 0

OA2 (integrator) and OA3 (inverter):

V2=−V1sR3C2,V3=−V2=V1sR3C2  ⇒  V1=sR3C2V3V_2 = -\frac{V_1}{sR_3C_2}, \qquad V_3 = -V_2 = \frac{V_1}{sR_3C_2} \;\Rightarrow\; V_1 = sR_3C_2V_3

Substituting V1V_1 into the KCL equation:

sR3C2V3(1R1+sC1)+V3R2=−VinR4V3(s2R3C1C2+sR3C2R1+1R2)=−VinR4\begin{aligned} sR_3C_2V_3\left(\frac{1}{R_1} + sC_1\right) + \frac{V_3}{R_2} &= -\frac{V_{in}}{R_4} \\ V_3\left(s^2R_3C_1C_2 + \frac{sR_3C_2}{R_1} + \frac{1}{R_2}\right) &= -\frac{V_{in}}{R_4} \end{aligned}

Dividing by R3C1C2R_3C_1C_2:

V3Vin=−1R3R4C1C2s2+sR1C1+1R2R3C1C2,V2Vin=−V3Vin\frac{V_3}{V_{in}} = \frac{-\dfrac{1}{R_3R_4C_1C_2}}{s^2 + \dfrac{s}{R_1C_1} + \dfrac{1}{R_2R_3C_1C_2}}, \qquad \frac{V_2}{V_{in}} = -\frac{V_3}{V_{in}}

Comparing with T(s)=±Kω02s2+(ω0/Q)s+ω02T(s) = \dfrac{\pm K\omega_0^2}{s^2 + (\omega_0/Q)s + \omega_0^2}:

ω0=1R2R3C1C2,ω0Q=1R1C1,K=R2R4 (dc gain)\omega_0 = \frac{1}{\sqrt{R_2R_3C_1C_2}}, \qquad \frac{\omega_0}{Q} = \frac{1}{R_1C_1}, \qquad K = \frac{R_2}{R_4}\ \text{(dc gain)}

V2V_2 is a non-inverting low-pass output and V3V_3 an inverting one; V1V_1 is a band-pass output.

Design: 2nd order Butterworth LPF, fc=5f_c = 5 kHz

Step 1: Parameters. For a 2nd order Butterworth filter the half-power frequency equals ω0\omega_0 and Q=1/2=0.7071Q = 1/\sqrt2 = 0.7071 (poles at 135∘135^\circ, from B(s)=s2+2s+1B(s) = s^2 + \sqrt2 s + 1).

ω0=2πfc=2π×5000=31,415.9 rad/s\omega_0 = 2\pi f_c = 2\pi \times 5000 = 31{,}415.9\ \text{rad/s}

No gain is specified, so take dc gain K=1K = 1:

T(s)=ω02s2+2 ω0s+ω02T(s) = \frac{\omega_0^2}{s^2 + \sqrt2\,\omega_0 s + \omega_0^2}

Design equations (choose C1=C2=CC_1 = C_2 = C, R2=R3=RR_2 = R_3 = R):

R=1ω0C,R1=QR=Qω0C,R4=R2K,r=any convenient valueR = \frac{1}{\omega_0 C}, \qquad R_1 = QR = \frac{Q}{\omega_0 C}, \qquad R_4 = \frac{R_2}{K}, \qquad r = \text{any convenient value}

Step 2: Element values with the given C1=C2=C=0.001 μC_1 = C_2 = C = 0.001\ \muF:

R2=R3=R=1ω0C=131,415.9×10−9=31.83 kΩR1=QR=0.7071×31.83=22.51 kΩR4=R2K=31.83 kΩr=10 kΩ\begin{aligned} R_2 = R_3 = R &= \frac{1}{\omega_0 C} = \frac{1}{31{,}415.9 \times 10^{-9}} = 31.83\ \text{k}\Omega \\ R_1 &= QR = 0.7071 \times 31.83 = 22.51\ \text{k}\Omega \\ R_4 &= \frac{R_2}{K} = 31.83\ \text{k}\Omega \\ r &= 10\ \text{k}\Omega \end{aligned}

(Equivalently: normalized design C=1C = 1 F, R2=R3=R4=1 ΩR_2 = R_3 = R_4 = 1\ \Omega, R1=0.7071 ΩR_1 = 0.7071\ \Omega, then frequency scale by kf=31,415.9k_f = 31{,}415.9 and impedance scale by km=1/(kf×10−9)=31,831k_m = 1/(k_f \times 10^{-9}) = 31{,}831.)

Answer: C1=C2=0.001 μC_1 = C_2 = 0.001\ \muF, R1=22.51R_1 = 22.51 kΩ\Omega, R2=R3=R4=31.83R_2 = R_3 = R_4 = 31.83 kΩ\Omega, r=10r = 10 kΩ\Omega; output at V2V_2, half-power frequency 5 kHz, unity dc gain.

  • 2070 Chaitra · 3+5 marks

Draw the circuit diagram and derive transfer function of Tow Thomas Biquad circuit. Design a low pass filter using Tow-Thomas Biquad circuit with poles at -500 ± j2449.49 and dc gain of 2. The final circuit should consist capacitors of value 0.1μF.

Answer

Tow-Thomas low-pass biquad

The Tow-Thomas biquad is a two-integrator-loop circuit using three op-amps: a lossy integrator, an ideal integrator and an inverter in a feedback loop. It gives low-pass and band-pass outputs at the same time, has low sensitivity, and lets ω0\omega_0, QQ and gain be tuned independently.

            R1 (sets Q)
          +--/\/\--+
          |   C1   |
          +---||---+
          |        |
Vin--R4---+--[OA1]-+--> V1 (band-pass)
          ^
          |  V1--R3-->[OA2 integrator, C2]--> V2 (LP)
          |  V2--r--->[OA3 inverter, r/r]---> V3=-V2
          |                                    |
          +------------------R2----------------+

All op-amp (+) inputs are grounded. OA1 is a lossy integrator (R1∥C1R_1 \parallel C_1 in feedback), OA2 an ideal integrator (C2C_2 in feedback), OA3 a unity-gain inverter.

Derivation (ideal op-amps, so each inverting input is a virtual ground):

KCL at the inverting input of OA1:

VinR4+V3R2+V1(1R1+sC1)=0\frac{V_{in}}{R_4} + \frac{V_3}{R_2} + V_1\left(\frac{1}{R_1} + sC_1\right) = 0

OA2 (integrator) and OA3 (inverter):

V2=−V1sR3C2,V3=−V2=V1sR3C2  ⇒  V1=sR3C2V3V_2 = -\frac{V_1}{sR_3C_2}, \qquad V_3 = -V_2 = \frac{V_1}{sR_3C_2} \;\Rightarrow\; V_1 = sR_3C_2V_3

Substituting V1V_1 into the KCL equation:

sR3C2V3(1R1+sC1)+V3R2=−VinR4V3(s2R3C1C2+sR3C2R1+1R2)=−VinR4\begin{aligned} sR_3C_2V_3\left(\frac{1}{R_1} + sC_1\right) + \frac{V_3}{R_2} &= -\frac{V_{in}}{R_4} \\ V_3\left(s^2R_3C_1C_2 + \frac{sR_3C_2}{R_1} + \frac{1}{R_2}\right) &= -\frac{V_{in}}{R_4} \end{aligned}

Dividing by R3C1C2R_3C_1C_2:

V3Vin=−1R3R4C1C2s2+sR1C1+1R2R3C1C2,V2Vin=−V3Vin\frac{V_3}{V_{in}} = \frac{-\dfrac{1}{R_3R_4C_1C_2}}{s^2 + \dfrac{s}{R_1C_1} + \dfrac{1}{R_2R_3C_1C_2}}, \qquad \frac{V_2}{V_{in}} = -\frac{V_3}{V_{in}}

Comparing with T(s)=±Kω02s2+(ω0/Q)s+ω02T(s) = \dfrac{\pm K\omega_0^2}{s^2 + (\omega_0/Q)s + \omega_0^2}:

ω0=1R2R3C1C2,ω0Q=1R1C1,K=R2R4 (dc gain)\omega_0 = \frac{1}{\sqrt{R_2R_3C_1C_2}}, \qquad \frac{\omega_0}{Q} = \frac{1}{R_1C_1}, \qquad K = \frac{R_2}{R_4}\ \text{(dc gain)}

V2V_2 is a non-inverting low-pass output and V3V_3 an inverting one; V1V_1 is a band-pass output.

Design

Step 1: ω0\omega_0 and QQ from the poles. Poles s=−σ±jωds = -\sigma \pm j\omega_d with σ=500\sigma = 500, ωd=2449.49\omega_d = 2449.49:

ω02=σ2+ωd2=5002+2449.492=6,250,001  ⇒  ω0≈2500 rad/sω0Q=2σ  ⇒  Q=ω02σ=25001000=2.5\begin{aligned} \omega_0^2 &= \sigma^2 + \omega_d^2 = 500^2 + 2449.49^2 = 6{,}250{,}001 \;\Rightarrow\; \omega_0 \approx 2500\ \text{rad/s} \\ \frac{\omega_0}{Q} &= 2\sigma \;\Rightarrow\; Q = \frac{\omega_0}{2\sigma} = \frac{2500}{1000} = 2.5 \end{aligned}

Required transfer function (dc gain K=2K = 2):

T(s)=2 ω02s2+2σs+ω02=2×6.25×106s2+1000 s+6.25×106T(s) = \frac{2\,\omega_0^2}{s^2 + 2\sigma s + \omega_0^2} = \frac{2 \times 6.25\times10^{6}}{s^2 + 1000\,s + 6.25\times10^{6}}

Design equations (choose C1=C2=CC_1 = C_2 = C, R2=R3=RR_2 = R_3 = R):

R=1ω0C,R1=QR=Qω0C,R4=R2K,r=any convenient valueR = \frac{1}{\omega_0 C}, \qquad R_1 = QR = \frac{Q}{\omega_0 C}, \qquad R_4 = \frac{R_2}{K}, \qquad r = \text{any convenient value}

Step 2: Element values. Given C1=C2=C=0.1 μC_1 = C_2 = C = 0.1\ \muF.

R2=R3=R=1ω0C=12500×0.1×10−6=4 kΩR1=QR=2.5×4 kΩ=10 kΩR4=R2K=4 kΩ2=2 kΩr=10 kΩ (inverter, equal resistors)\begin{aligned} R_2 = R_3 = R &= \frac{1}{\omega_0 C} = \frac{1}{2500 \times 0.1\times10^{-6}} = 4\ \text{k}\Omega \\ R_1 &= QR = 2.5 \times 4\ \text{k}\Omega = 10\ \text{k}\Omega \\ R_4 &= \frac{R_2}{K} = \frac{4\ \text{k}\Omega}{2} = 2\ \text{k}\Omega \\ r &= 10\ \text{k}\Omega \ \text{(inverter, equal resistors)} \end{aligned}

Final circuit: Tow-Thomas biquad (figure above) with C1=C2=0.1 μFC_1 = C_2 = 0.1\ \mu\text{F}, R1=10 kΩR_1 = 10\ \text{k}\Omega, R2=R3=4 kΩR_2 = R_3 = 4\ \text{k}\Omega, R4=2 kΩR_4 = 2\ \text{k}\Omega, r=10 kΩr = 10\ \text{k}\Omega; take the output at V2V_2 (OA2 output) for a positive dc gain of 2.

Answer: C=0.1 μFC = 0.1\ \mu\text{F}, R1=10 kΩR_1 = 10\ \text{k}\Omega, R2=R3=4 kΩR_2 = R_3 = 4\ \text{k}\Omega, R4=2 kΩR_4 = 2\ \text{k}\Omega, r=10 kΩr = 10\ \text{k}\Omega (all practical values).

  • 2069 Chaitra · 8 marks

Draw the circuit diagram of Tow thomas biquad low pass filter and derive its transfer function. Design a second order low pass filter using Tow Thomas biquad circuit having poles at -750 ± j661.44 and dc gain of 2. Use capacitor of value 0.01μF in your design.

Answer

Tow-Thomas low-pass biquad

The Tow-Thomas biquad is a two-integrator-loop circuit using three op-amps: a lossy integrator, an ideal integrator and an inverter in a feedback loop. It gives low-pass and band-pass outputs at the same time, has low sensitivity, and lets ω0\omega_0, QQ and gain be tuned independently.

            R1 (sets Q)
          +--/\/\--+
          |   C1   |
          +---||---+
          |        |
Vin--R4---+--[OA1]-+--> V1 (band-pass)
          ^
          |  V1--R3-->[OA2 integrator, C2]--> V2 (LP)
          |  V2--r--->[OA3 inverter, r/r]---> V3=-V2
          |                                    |
          +------------------R2----------------+

All op-amp (+) inputs are grounded. OA1 is a lossy integrator (R1∥C1R_1 \parallel C_1 in feedback), OA2 an ideal integrator (C2C_2 in feedback), OA3 a unity-gain inverter.

Derivation (ideal op-amps, so each inverting input is a virtual ground):

KCL at the inverting input of OA1:

VinR4+V3R2+V1(1R1+sC1)=0\frac{V_{in}}{R_4} + \frac{V_3}{R_2} + V_1\left(\frac{1}{R_1} + sC_1\right) = 0

OA2 (integrator) and OA3 (inverter):

V2=−V1sR3C2,V3=−V2=V1sR3C2  ⇒  V1=sR3C2V3V_2 = -\frac{V_1}{sR_3C_2}, \qquad V_3 = -V_2 = \frac{V_1}{sR_3C_2} \;\Rightarrow\; V_1 = sR_3C_2V_3

Substituting V1V_1 into the KCL equation:

sR3C2V3(1R1+sC1)+V3R2=−VinR4V3(s2R3C1C2+sR3C2R1+1R2)=−VinR4\begin{aligned} sR_3C_2V_3\left(\frac{1}{R_1} + sC_1\right) + \frac{V_3}{R_2} &= -\frac{V_{in}}{R_4} \\ V_3\left(s^2R_3C_1C_2 + \frac{sR_3C_2}{R_1} + \frac{1}{R_2}\right) &= -\frac{V_{in}}{R_4} \end{aligned}

Dividing by R3C1C2R_3C_1C_2:

V3Vin=−1R3R4C1C2s2+sR1C1+1R2R3C1C2,V2Vin=−V3Vin\frac{V_3}{V_{in}} = \frac{-\dfrac{1}{R_3R_4C_1C_2}}{s^2 + \dfrac{s}{R_1C_1} + \dfrac{1}{R_2R_3C_1C_2}}, \qquad \frac{V_2}{V_{in}} = -\frac{V_3}{V_{in}}

Comparing with T(s)=±Kω02s2+(ω0/Q)s+ω02T(s) = \dfrac{\pm K\omega_0^2}{s^2 + (\omega_0/Q)s + \omega_0^2}:

ω0=1R2R3C1C2,ω0Q=1R1C1,K=R2R4 (dc gain)\omega_0 = \frac{1}{\sqrt{R_2R_3C_1C_2}}, \qquad \frac{\omega_0}{Q} = \frac{1}{R_1C_1}, \qquad K = \frac{R_2}{R_4}\ \text{(dc gain)}

V2V_2 is a non-inverting low-pass output and V3V_3 an inverting one; V1V_1 is a band-pass output.

Design

Step 1: ω0\omega_0 and QQ from the poles. Poles s=−σ±jωds = -\sigma \pm j\omega_d with σ=750\sigma = 750, ωd=661.44\omega_d = 661.44:

ω02=σ2+ωd2=7502+661.442=1,000,003  ⇒  ω0≈1000 rad/sω0Q=2σ  ⇒  Q=ω02σ=10001500=0.6667\begin{aligned} \omega_0^2 &= \sigma^2 + \omega_d^2 = 750^2 + 661.44^2 = 1{,}000{,}003 \;\Rightarrow\; \omega_0 \approx 1000\ \text{rad/s} \\ \frac{\omega_0}{Q} &= 2\sigma \;\Rightarrow\; Q = \frac{\omega_0}{2\sigma} = \frac{1000}{1500} = 0.6667 \end{aligned}

Required transfer function (dc gain K=2K = 2):

T(s)=2 ω02s2+2σs+ω02=2×106s2+1500 s+106T(s) = \frac{2\,\omega_0^2}{s^2 + 2\sigma s + \omega_0^2} = \frac{2 \times 10^{6}}{s^2 + 1500\,s + 10^{6}}

Design equations (choose C1=C2=CC_1 = C_2 = C, R2=R3=RR_2 = R_3 = R):

R=1ω0C,R1=QR=Qω0C,R4=R2K,r=any convenient valueR = \frac{1}{\omega_0 C}, \qquad R_1 = QR = \frac{Q}{\omega_0 C}, \qquad R_4 = \frac{R_2}{K}, \qquad r = \text{any convenient value}

Step 2: Element values. Given C1=C2=C=0.01 μC_1 = C_2 = C = 0.01\ \muF.

R2=R3=R=1ω0C=11000×0.01×10−6=100 kΩR1=QR=0.6667×100 kΩ=66.67 kΩR4=R2K=100 kΩ2=50 kΩr=10 kΩ (inverter, equal resistors)\begin{aligned} R_2 = R_3 = R &= \frac{1}{\omega_0 C} = \frac{1}{1000 \times 0.01\times10^{-6}} = 100\ \text{k}\Omega \\ R_1 &= QR = 0.6667 \times 100\ \text{k}\Omega = 66.67\ \text{k}\Omega \\ R_4 &= \frac{R_2}{K} = \frac{100\ \text{k}\Omega}{2} = 50\ \text{k}\Omega \\ r &= 10\ \text{k}\Omega \ \text{(inverter, equal resistors)} \end{aligned}

Final circuit: Tow-Thomas biquad (figure above) with C1=C2=0.01 μFC_1 = C_2 = 0.01\ \mu\text{F}, R1=66.67 kΩR_1 = 66.67\ \text{k}\Omega, R2=R3=100 kΩR_2 = R_3 = 100\ \text{k}\Omega, R4=50 kΩR_4 = 50\ \text{k}\Omega, r=10 kΩr = 10\ \text{k}\Omega; take the output at V2V_2 (OA2 output) for a positive dc gain of 2.

Answer: C=0.01 μFC = 0.01\ \mu\text{F}, R1=66.67 kΩR_1 = 66.67\ \text{k}\Omega, R2=R3=100 kΩR_2 = R_3 = 100\ \text{k}\Omega, R4=50 kΩR_4 = 50\ \text{k}\Omega, r=10 kΩr = 10\ \text{k}\Omega (all practical values).

  • 2080 Baisakh · 4+4 marks

Derive the transfer function of Tow-Thomas lowpass biquad filter and design a lowpass filter having poles at -400 ± j3979.95 and dc gain of 4 with practically realizable elements.

Answer

Tow-Thomas low-pass biquad

The Tow-Thomas biquad is a two-integrator-loop circuit using three op-amps: a lossy integrator, an ideal integrator and an inverter in a feedback loop. It gives low-pass and band-pass outputs at the same time, has low sensitivity, and lets ω0\omega_0, QQ and gain be tuned independently.

            R1 (sets Q)
          +--/\/\--+
          |   C1   |
          +---||---+
          |        |
Vin--R4---+--[OA1]-+--> V1 (band-pass)
          ^
          |  V1--R3-->[OA2 integrator, C2]--> V2 (LP)
          |  V2--r--->[OA3 inverter, r/r]---> V3=-V2
          |                                    |
          +------------------R2----------------+

All op-amp (+) inputs are grounded. OA1 is a lossy integrator (R1∥C1R_1 \parallel C_1 in feedback), OA2 an ideal integrator (C2C_2 in feedback), OA3 a unity-gain inverter.

Derivation (ideal op-amps, so each inverting input is a virtual ground):

KCL at the inverting input of OA1:

VinR4+V3R2+V1(1R1+sC1)=0\frac{V_{in}}{R_4} + \frac{V_3}{R_2} + V_1\left(\frac{1}{R_1} + sC_1\right) = 0

OA2 (integrator) and OA3 (inverter):

V2=−V1sR3C2,V3=−V2=V1sR3C2  ⇒  V1=sR3C2V3V_2 = -\frac{V_1}{sR_3C_2}, \qquad V_3 = -V_2 = \frac{V_1}{sR_3C_2} \;\Rightarrow\; V_1 = sR_3C_2V_3

Substituting V1V_1 into the KCL equation:

sR3C2V3(1R1+sC1)+V3R2=−VinR4V3(s2R3C1C2+sR3C2R1+1R2)=−VinR4\begin{aligned} sR_3C_2V_3\left(\frac{1}{R_1} + sC_1\right) + \frac{V_3}{R_2} &= -\frac{V_{in}}{R_4} \\ V_3\left(s^2R_3C_1C_2 + \frac{sR_3C_2}{R_1} + \frac{1}{R_2}\right) &= -\frac{V_{in}}{R_4} \end{aligned}

Dividing by R3C1C2R_3C_1C_2:

V3Vin=−1R3R4C1C2s2+sR1C1+1R2R3C1C2,V2Vin=−V3Vin\frac{V_3}{V_{in}} = \frac{-\dfrac{1}{R_3R_4C_1C_2}}{s^2 + \dfrac{s}{R_1C_1} + \dfrac{1}{R_2R_3C_1C_2}}, \qquad \frac{V_2}{V_{in}} = -\frac{V_3}{V_{in}}

Comparing with T(s)=±Kω02s2+(ω0/Q)s+ω02T(s) = \dfrac{\pm K\omega_0^2}{s^2 + (\omega_0/Q)s + \omega_0^2}:

ω0=1R2R3C1C2,ω0Q=1R1C1,K=R2R4 (dc gain)\omega_0 = \frac{1}{\sqrt{R_2R_3C_1C_2}}, \qquad \frac{\omega_0}{Q} = \frac{1}{R_1C_1}, \qquad K = \frac{R_2}{R_4}\ \text{(dc gain)}

V2V_2 is a non-inverting low-pass output and V3V_3 an inverting one; V1V_1 is a band-pass output.

Design

Step 1: ω0\omega_0 and QQ from the poles. Poles s=−σ±jωds = -\sigma \pm j\omega_d with σ=400\sigma = 400, ωd=3979.95\omega_d = 3979.95:

ω02=σ2+ωd2=4002+3979.952=16,000,002  ⇒  ω0≈4000 rad/sω0Q=2σ  ⇒  Q=ω02σ=4000800=5\begin{aligned} \omega_0^2 &= \sigma^2 + \omega_d^2 = 400^2 + 3979.95^2 = 16{,}000{,}002 \;\Rightarrow\; \omega_0 \approx 4000\ \text{rad/s} \\ \frac{\omega_0}{Q} &= 2\sigma \;\Rightarrow\; Q = \frac{\omega_0}{2\sigma} = \frac{4000}{800} = 5 \end{aligned}

Required transfer function (dc gain K=4K = 4):

T(s)=4 ω02s2+2σs+ω02=4×1.6×107s2+800 s+1.6×107T(s) = \frac{4\,\omega_0^2}{s^2 + 2\sigma s + \omega_0^2} = \frac{4 \times 1.6\times10^{7}}{s^2 + 800\,s + 1.6\times10^{7}}

Design equations (choose C1=C2=CC_1 = C_2 = C, R2=R3=RR_2 = R_3 = R):

R=1ω0C,R1=QR=Qω0C,R4=R2K,r=any convenient valueR = \frac{1}{\omega_0 C}, \qquad R_1 = QR = \frac{Q}{\omega_0 C}, \qquad R_4 = \frac{R_2}{K}, \qquad r = \text{any convenient value}

Step 2: Element values. Choose C1=C2=C=0.01 μC_1 = C_2 = C = 0.01\ \muF so that all resistors fall in the kΩ\Omega range.

R2=R3=R=1ω0C=14000×0.01×10−6=25 kΩR1=QR=5×25 kΩ=125 kΩR4=R2K=25 kΩ4=6.25 kΩr=10 kΩ (inverter, equal resistors)\begin{aligned} R_2 = R_3 = R &= \frac{1}{\omega_0 C} = \frac{1}{4000 \times 0.01\times10^{-6}} = 25\ \text{k}\Omega \\ R_1 &= QR = 5 \times 25\ \text{k}\Omega = 125\ \text{k}\Omega \\ R_4 &= \frac{R_2}{K} = \frac{25\ \text{k}\Omega}{4} = 6.25\ \text{k}\Omega \\ r &= 10\ \text{k}\Omega \ \text{(inverter, equal resistors)} \end{aligned}

Final circuit: Tow-Thomas biquad (figure above) with C1=C2=0.01 μFC_1 = C_2 = 0.01\ \mu\text{F}, R1=125 kΩR_1 = 125\ \text{k}\Omega, R2=R3=25 kΩR_2 = R_3 = 25\ \text{k}\Omega, R4=6.25 kΩR_4 = 6.25\ \text{k}\Omega, r=10 kΩr = 10\ \text{k}\Omega; take the output at V2V_2 (OA2 output) for a positive dc gain of 4.

Answer: C=0.01 μFC = 0.01\ \mu\text{F}, R1=125 kΩR_1 = 125\ \text{k}\Omega, R2=R3=25 kΩR_2 = R_3 = 25\ \text{k}\Omega, R4=6.25 kΩR_4 = 6.25\ \text{k}\Omega, r=10 kΩr = 10\ \text{k}\Omega (all practical values).

  • 2078 Bhadra · 4+4 marks

Derive the transfer function of Tow-Thomas low pass biquad. Design a lowpass filter having poles at -24000 ± j32000 and dc gain of 2, with practically suitable elements.

Answer

Tow-Thomas low-pass biquad

The Tow-Thomas biquad is a two-integrator-loop circuit using three op-amps: a lossy integrator, an ideal integrator and an inverter in a feedback loop. It gives low-pass and band-pass outputs at the same time, has low sensitivity, and lets ω0\omega_0, QQ and gain be tuned independently.

            R1 (sets Q)
          +--/\/\--+
          |   C1   |
          +---||---+
          |        |
Vin--R4---+--[OA1]-+--> V1 (band-pass)
          ^
          |  V1--R3-->[OA2 integrator, C2]--> V2 (LP)
          |  V2--r--->[OA3 inverter, r/r]---> V3=-V2
          |                                    |
          +------------------R2----------------+

All op-amp (+) inputs are grounded. OA1 is a lossy integrator (R1∥C1R_1 \parallel C_1 in feedback), OA2 an ideal integrator (C2C_2 in feedback), OA3 a unity-gain inverter.

Derivation (ideal op-amps, so each inverting input is a virtual ground):

KCL at the inverting input of OA1:

VinR4+V3R2+V1(1R1+sC1)=0\frac{V_{in}}{R_4} + \frac{V_3}{R_2} + V_1\left(\frac{1}{R_1} + sC_1\right) = 0

OA2 (integrator) and OA3 (inverter):

V2=−V1sR3C2,V3=−V2=V1sR3C2  ⇒  V1=sR3C2V3V_2 = -\frac{V_1}{sR_3C_2}, \qquad V_3 = -V_2 = \frac{V_1}{sR_3C_2} \;\Rightarrow\; V_1 = sR_3C_2V_3

Substituting V1V_1 into the KCL equation:

sR3C2V3(1R1+sC1)+V3R2=−VinR4V3(s2R3C1C2+sR3C2R1+1R2)=−VinR4\begin{aligned} sR_3C_2V_3\left(\frac{1}{R_1} + sC_1\right) + \frac{V_3}{R_2} &= -\frac{V_{in}}{R_4} \\ V_3\left(s^2R_3C_1C_2 + \frac{sR_3C_2}{R_1} + \frac{1}{R_2}\right) &= -\frac{V_{in}}{R_4} \end{aligned}

Dividing by R3C1C2R_3C_1C_2:

V3Vin=−1R3R4C1C2s2+sR1C1+1R2R3C1C2,V2Vin=−V3Vin\frac{V_3}{V_{in}} = \frac{-\dfrac{1}{R_3R_4C_1C_2}}{s^2 + \dfrac{s}{R_1C_1} + \dfrac{1}{R_2R_3C_1C_2}}, \qquad \frac{V_2}{V_{in}} = -\frac{V_3}{V_{in}}

Comparing with T(s)=±Kω02s2+(ω0/Q)s+ω02T(s) = \dfrac{\pm K\omega_0^2}{s^2 + (\omega_0/Q)s + \omega_0^2}:

ω0=1R2R3C1C2,ω0Q=1R1C1,K=R2R4 (dc gain)\omega_0 = \frac{1}{\sqrt{R_2R_3C_1C_2}}, \qquad \frac{\omega_0}{Q} = \frac{1}{R_1C_1}, \qquad K = \frac{R_2}{R_4}\ \text{(dc gain)}

V2V_2 is a non-inverting low-pass output and V3V_3 an inverting one; V1V_1 is a band-pass output.

Design

Step 1: ω0\omega_0 and QQ from the poles. Poles s=−σ±jωds = -\sigma \pm j\omega_d with σ=24000\sigma = 24000, ωd=32000\omega_d = 32000:

ω02=σ2+ωd2=240002+320002=1.6×109  ⇒  ω0≈40,000 rad/sω0Q=2σ  ⇒  Q=ω02σ=4000048000=0.8333\begin{aligned} \omega_0^2 &= \sigma^2 + \omega_d^2 = 24000^2 + 32000^2 = 1.6\times10^9 \;\Rightarrow\; \omega_0 \approx 40{,}000\ \text{rad/s} \\ \frac{\omega_0}{Q} &= 2\sigma \;\Rightarrow\; Q = \frac{\omega_0}{2\sigma} = \frac{40000}{48000} = 0.8333 \end{aligned}

Required transfer function (dc gain K=2K = 2):

T(s)=2 ω02s2+2σs+ω02=2×1.6×109s2+48000 s+1.6×109T(s) = \frac{2\,\omega_0^2}{s^2 + 2\sigma s + \omega_0^2} = \frac{2 \times 1.6\times10^{9}}{s^2 + 48000\,s + 1.6\times10^{9}}

Design equations (choose C1=C2=CC_1 = C_2 = C, R2=R3=RR_2 = R_3 = R):

R=1ω0C,R1=QR=Qω0C,R4=R2K,r=any convenient valueR = \frac{1}{\omega_0 C}, \qquad R_1 = QR = \frac{Q}{\omega_0 C}, \qquad R_4 = \frac{R_2}{K}, \qquad r = \text{any convenient value}

Step 2: Element values. Choose C1=C2=C=0.001 μC_1 = C_2 = C = 0.001\ \muF (1 nF) so that the resistors are in the kΩ\Omega range.

R2=R3=R=1ω0C=140,000×0.001×10−6=25 kΩR1=QR=0.8333×25 kΩ=20.83 kΩR4=R2K=25 kΩ2=12.5 kΩr=10 kΩ (inverter, equal resistors)\begin{aligned} R_2 = R_3 = R &= \frac{1}{\omega_0 C} = \frac{1}{40{,}000 \times 0.001\times10^{-6}} = 25\ \text{k}\Omega \\ R_1 &= QR = 0.8333 \times 25\ \text{k}\Omega = 20.83\ \text{k}\Omega \\ R_4 &= \frac{R_2}{K} = \frac{25\ \text{k}\Omega}{2} = 12.5\ \text{k}\Omega \\ r &= 10\ \text{k}\Omega \ \text{(inverter, equal resistors)} \end{aligned}

Final circuit: Tow-Thomas biquad (figure above) with C1=C2=0.001 μFC_1 = C_2 = 0.001\ \mu\text{F}, R1=20.83 kΩR_1 = 20.83\ \text{k}\Omega, R2=R3=25 kΩR_2 = R_3 = 25\ \text{k}\Omega, R4=12.5 kΩR_4 = 12.5\ \text{k}\Omega, r=10 kΩr = 10\ \text{k}\Omega; take the output at V2V_2 (OA2 output) for a positive dc gain of 2.

Answer: C=0.001 μFC = 0.001\ \mu\text{F}, R1=20.83 kΩR_1 = 20.83\ \text{k}\Omega, R2=R3=25 kΩR_2 = R_3 = 25\ \text{k}\Omega, R4=12.5 kΩR_4 = 12.5\ \text{k}\Omega, r=10 kΩr = 10\ \text{k}\Omega (all practical values).

  • 2076 Asoj · 4+4 marks

Draw the circuit diagram of Tow Thomas low pass circuit and derive its transfer function. Design a second order low pass filter with poles at -4000 ± j39799.4975 and DC Gain of 1.5 using a Tow Thomas Biquad Circuit. Your final circuit design should have capacitors of value 0.001uF.

Answer

Tow-Thomas low-pass biquad

The Tow-Thomas biquad is a two-integrator-loop circuit using three op-amps: a lossy integrator, an ideal integrator and an inverter in a feedback loop. It gives low-pass and band-pass outputs at the same time, has low sensitivity, and lets ω0\omega_0, QQ and gain be tuned independently.

            R1 (sets Q)
          +--/\/\--+
          |   C1   |
          +---||---+
          |        |
Vin--R4---+--[OA1]-+--> V1 (band-pass)
          ^
          |  V1--R3-->[OA2 integrator, C2]--> V2 (LP)
          |  V2--r--->[OA3 inverter, r/r]---> V3=-V2
          |                                    |
          +------------------R2----------------+

All op-amp (+) inputs are grounded. OA1 is a lossy integrator (R1∥C1R_1 \parallel C_1 in feedback), OA2 an ideal integrator (C2C_2 in feedback), OA3 a unity-gain inverter.

Derivation (ideal op-amps, so each inverting input is a virtual ground):

KCL at the inverting input of OA1:

VinR4+V3R2+V1(1R1+sC1)=0\frac{V_{in}}{R_4} + \frac{V_3}{R_2} + V_1\left(\frac{1}{R_1} + sC_1\right) = 0

OA2 (integrator) and OA3 (inverter):

V2=−V1sR3C2,V3=−V2=V1sR3C2  ⇒  V1=sR3C2V3V_2 = -\frac{V_1}{sR_3C_2}, \qquad V_3 = -V_2 = \frac{V_1}{sR_3C_2} \;\Rightarrow\; V_1 = sR_3C_2V_3

Substituting V1V_1 into the KCL equation:

sR3C2V3(1R1+sC1)+V3R2=−VinR4V3(s2R3C1C2+sR3C2R1+1R2)=−VinR4\begin{aligned} sR_3C_2V_3\left(\frac{1}{R_1} + sC_1\right) + \frac{V_3}{R_2} &= -\frac{V_{in}}{R_4} \\ V_3\left(s^2R_3C_1C_2 + \frac{sR_3C_2}{R_1} + \frac{1}{R_2}\right) &= -\frac{V_{in}}{R_4} \end{aligned}

Dividing by R3C1C2R_3C_1C_2:

V3Vin=−1R3R4C1C2s2+sR1C1+1R2R3C1C2,V2Vin=−V3Vin\frac{V_3}{V_{in}} = \frac{-\dfrac{1}{R_3R_4C_1C_2}}{s^2 + \dfrac{s}{R_1C_1} + \dfrac{1}{R_2R_3C_1C_2}}, \qquad \frac{V_2}{V_{in}} = -\frac{V_3}{V_{in}}

Comparing with T(s)=±Kω02s2+(ω0/Q)s+ω02T(s) = \dfrac{\pm K\omega_0^2}{s^2 + (\omega_0/Q)s + \omega_0^2}:

ω0=1R2R3C1C2,ω0Q=1R1C1,K=R2R4 (dc gain)\omega_0 = \frac{1}{\sqrt{R_2R_3C_1C_2}}, \qquad \frac{\omega_0}{Q} = \frac{1}{R_1C_1}, \qquad K = \frac{R_2}{R_4}\ \text{(dc gain)}

V2V_2 is a non-inverting low-pass output and V3V_3 an inverting one; V1V_1 is a band-pass output.

Design

Step 1: ω0\omega_0 and QQ from the poles. Poles s=−σ±jωds = -\sigma \pm j\omega_d with σ=4000\sigma = 4000, ωd=39799.4975\omega_d = 39799.4975:

ω02=σ2+ωd2=40002+39799.49752=1.6×109  ⇒  ω0≈40,000 rad/sω0Q=2σ  ⇒  Q=ω02σ=400008000=5\begin{aligned} \omega_0^2 &= \sigma^2 + \omega_d^2 = 4000^2 + 39799.4975^2 = 1.6\times10^9 \;\Rightarrow\; \omega_0 \approx 40{,}000\ \text{rad/s} \\ \frac{\omega_0}{Q} &= 2\sigma \;\Rightarrow\; Q = \frac{\omega_0}{2\sigma} = \frac{40000}{8000} = 5 \end{aligned}

Required transfer function (dc gain K=1.5K = 1.5):

T(s)=1.5 ω02s2+2σs+ω02=1.5×1.6×109s2+8000 s+1.6×109T(s) = \frac{1.5\,\omega_0^2}{s^2 + 2\sigma s + \omega_0^2} = \frac{1.5 \times 1.6\times10^{9}}{s^2 + 8000\,s + 1.6\times10^{9}}

Design equations (choose C1=C2=CC_1 = C_2 = C, R2=R3=RR_2 = R_3 = R):

R=1ω0C,R1=QR=Qω0C,R4=R2K,r=any convenient valueR = \frac{1}{\omega_0 C}, \qquad R_1 = QR = \frac{Q}{\omega_0 C}, \qquad R_4 = \frac{R_2}{K}, \qquad r = \text{any convenient value}

Step 2: Element values. Given C1=C2=C=0.001 μC_1 = C_2 = C = 0.001\ \muF.

R2=R3=R=1ω0C=140,000×0.001×10−6=25 kΩR1=QR=5×25 kΩ=125 kΩR4=R2K=25 kΩ1.5=16.67 kΩr=10 kΩ (inverter, equal resistors)\begin{aligned} R_2 = R_3 = R &= \frac{1}{\omega_0 C} = \frac{1}{40{,}000 \times 0.001\times10^{-6}} = 25\ \text{k}\Omega \\ R_1 &= QR = 5 \times 25\ \text{k}\Omega = 125\ \text{k}\Omega \\ R_4 &= \frac{R_2}{K} = \frac{25\ \text{k}\Omega}{1.5} = 16.67\ \text{k}\Omega \\ r &= 10\ \text{k}\Omega \ \text{(inverter, equal resistors)} \end{aligned}

Final circuit: Tow-Thomas biquad (figure above) with C1=C2=0.001 μFC_1 = C_2 = 0.001\ \mu\text{F}, R1=125 kΩR_1 = 125\ \text{k}\Omega, R2=R3=25 kΩR_2 = R_3 = 25\ \text{k}\Omega, R4=16.67 kΩR_4 = 16.67\ \text{k}\Omega, r=10 kΩr = 10\ \text{k}\Omega; take the output at V2V_2 (OA2 output) for a positive dc gain of 1.5.

Answer: C=0.001 μFC = 0.001\ \mu\text{F}, R1=125 kΩR_1 = 125\ \text{k}\Omega, R2=R3=25 kΩR_2 = R_3 = 25\ \text{k}\Omega, R4=16.67 kΩR_4 = 16.67\ \text{k}\Omega, r=10 kΩr = 10\ \text{k}\Omega (all practical values).

  • 2072 Kartik · 5+4 marks

Draw the circuit diagram of Sallen-Key low pass filter and derive its transfer function. Design second order butterworth low pass filter having half power frequency of 10 KHz using Sallen Key biquad. In your final design the value of capacitors must be 0.01μF and feedback resistors should also be equal (Refer table 1).

Answer

Sallen-Key low-pass circuit and transfer function

The Sallen-Key low-pass biquad uses one op-amp wired as a non-inverting amplifier of gain K=1+RB/RAK = 1 + R_B/R_A, two resistors R1,R2R_1, R_2 in series, a capacitor C1C_1 fed back from the output to node A, and a grounded capacitor C2C_2 at node B.

              C1 (feedback)
        +-----||-------------+
        |                    |
Vin -R1-+-(A)- R2 -+-(B)--|+\ |
                   |      |  >+---- Vo
                  === C2 +|-/ |
                   |     |    |
                  GND    +-RB-+
                         |
                         RA
                         |
                        GND

Derivation (ideal op-amp, so Vo=KVBV_o = K V_B and no current enters the + input):

Node B: the current through R2R_2 flows into C2C_2:

VA−VBR2=sC2VB  ⇒  VA=VB(1+sR2C2)\frac{V_A - V_B}{R_2} = sC_2 V_B \;\Rightarrow\; V_A = V_B(1 + sR_2C_2)

Node A (KCL):

Vin−VAR1=VA−VBR2+sC1(VA−Vo)\frac{V_{in} - V_A}{R_1} = \frac{V_A - V_B}{R_2} + sC_1 (V_A - V_o)

Substituting VAV_A and VB=Vo/KV_B = V_o/K and simplifying:

T(s)=VoVin=KR1R2C1C2s2+s(1R1C1+1R2C1+1−KR2C2)+1R1R2C1C2T(s) = \frac{V_o}{V_{in}} = \frac{\dfrac{K}{R_1R_2C_1C_2}}{s^2 + s\left(\dfrac{1}{R_1C_1} + \dfrac{1}{R_2C_1} + \dfrac{1-K}{R_2C_2}\right) + \dfrac{1}{R_1R_2C_1C_2}}

Comparing with T(s)=Kωo2s2+(ωo/Q)s+ωo2T(s) = \dfrac{K\omega_o^2}{s^2 + (\omega_o/Q)s + \omega_o^2}:

ωo=1R1R2C1C2ωoQ=1R1C1+1R2C1+1−KR2C2\begin{aligned} \omega_o &= \frac{1}{\sqrt{R_1R_2C_1C_2}} \\ \frac{\omega_o}{Q} &= \frac{1}{R_1C_1} + \frac{1}{R_2C_1} + \frac{1-K}{R_2C_2} \end{aligned}

DC gain =K= K.

Design: 2nd-order Butterworth, fc=10f_c = 10 kHz

From Table 1, the normalized 2nd-order Butterworth function is

T(s)=1s2+2 s+1  ⇒  ωo=1,  Q=12=0.7071T(s) = \frac{1}{s^2 + \sqrt{2}\,s + 1} \;\Rightarrow\; \omega_o = 1,\; Q = \frac{1}{\sqrt{2}} = 0.7071

For a Butterworth filter the half-power frequency equals ωo\omega_o.

Equal-element design (Design 1): take normalized R1=R2=1 ΩR_1 = R_2 = 1\ \Omega, C1=C2=1C_1 = C_2 = 1 F. Then ωo=1\omega_o = 1 rad/s and

1Q=1+1+(1−K)=3−K  ⇒  K=3−1Q\frac{1}{Q} = 1 + 1 + (1 - K) = 3 - K \;\Rightarrow\; K = 3 - \frac{1}{Q} K=3−2=1.586  ⇒  RBRA=K−1=0.586K = 3 - \sqrt{2} = 1.586 \;\Rightarrow\; \frac{R_B}{R_A} = K - 1 = 0.586

Denormalization:

kf=2π×10 000=62 831.85 rad/sC=Cnkfkm⇒km=162 831.85×0.01×10−6=1591.55R1=R2=km×1=1591.55 Ω≈1.59 kΩ\begin{aligned} k_f &= 2\pi \times 10\,000 = 62\,831.85\ \text{rad/s} \\ C &= \frac{C_n}{k_f k_m} \Rightarrow k_m = \frac{1}{62\,831.85 \times 0.01\times10^{-6}} = 1591.55 \\ R_1 = R_2 &= k_m \times 1 = 1591.55\ \Omega \approx 1.59\ \text{k}\Omega \end{aligned}

Choose RA=10 kΩR_A = 10\ \text{k}\Omega, so RB=0.586×10=5.86 kΩR_B = 0.586 \times 10 = 5.86\ \text{k}\Omega.

ElementValue
R1=R2R_1 = R_21.59 kΩ
C1=C2C_1 = C_20.01 μF
RAR_A10 kΩ
RBR_B5.86 kΩ
DC gain KK1.586 (4 dB)

Answer: R1=R2=1.59 kΩR_1 = R_2 = 1.59\ \text{k}\Omega, C1=C2=0.01 μFC_1 = C_2 = 0.01\ \mu\text{F}, RA=10 kΩR_A = 10\ \text{k}\Omega, RB=5.86 kΩR_B = 5.86\ \text{k}\Omega; this gives fc=10f_c = 10 kHz with Q=0.707Q = 0.707.

If unity overall gain is needed, use the input divider of gain α=1/1.586=0.631\alpha = 1/1.586 = 0.631: R1a=1.59/0.631=2.52 kΩR_{1a} = 1.59/0.631 = 2.52\ \text{k}\Omega and R1b=1.59/0.369=4.31 kΩR_{1b} = 1.59/0.369 = 4.31\ \text{k}\Omega.

  • 2075 Asoj · 4+4 marks

Derive transfer function of Sallen Key low pass filter. Design second order Butterworth low pass filter using Sallen Key biquad. In your final design the values of capacitor must be 0.01μF and feedback resistors should also be equal. [Use Table 1]

Answer

Transfer function of the Sallen-Key low-pass filter

The Sallen-Key low-pass biquad uses one op-amp wired as a non-inverting amplifier of gain K=1+RB/RAK = 1 + R_B/R_A, two resistors R1,R2R_1, R_2 in series, a capacitor C1C_1 fed back from the output to node A, and a grounded capacitor C2C_2 at node B.

              C1 (feedback)
        +-----||-------------+
        |                    |
Vin -R1-+-(A)- R2 -+-(B)--|+\ |
                   |      |  >+---- Vo
                  === C2 +|-/ |
                   |     |    |
                  GND    +-RB-+
                         |
                         RA
                         |
                        GND

Derivation (ideal op-amp, so Vo=KVBV_o = K V_B and no current enters the + input):

Node B: the current through R2R_2 flows into C2C_2:

VA−VBR2=sC2VB  ⇒  VA=VB(1+sR2C2)\frac{V_A - V_B}{R_2} = sC_2 V_B \;\Rightarrow\; V_A = V_B(1 + sR_2C_2)

Node A (KCL):

Vin−VAR1=VA−VBR2+sC1(VA−Vo)\frac{V_{in} - V_A}{R_1} = \frac{V_A - V_B}{R_2} + sC_1 (V_A - V_o)

Substituting VAV_A and VB=Vo/KV_B = V_o/K and simplifying:

T(s)=VoVin=KR1R2C1C2s2+s(1R1C1+1R2C1+1−KR2C2)+1R1R2C1C2T(s) = \frac{V_o}{V_{in}} = \frac{\dfrac{K}{R_1R_2C_1C_2}}{s^2 + s\left(\dfrac{1}{R_1C_1} + \dfrac{1}{R_2C_1} + \dfrac{1-K}{R_2C_2}\right) + \dfrac{1}{R_1R_2C_1C_2}}

Comparing with T(s)=Kωo2s2+(ωo/Q)s+ωo2T(s) = \dfrac{K\omega_o^2}{s^2 + (\omega_o/Q)s + \omega_o^2}:

ωo=1R1R2C1C2ωoQ=1R1C1+1R2C1+1−KR2C2\begin{aligned} \omega_o &= \frac{1}{\sqrt{R_1R_2C_1C_2}} \\ \frac{\omega_o}{Q} &= \frac{1}{R_1C_1} + \frac{1}{R_2C_1} + \frac{1-K}{R_2C_2} \end{aligned}

DC gain =K= K.

Design: 2nd-order Butterworth with C=0.01 μC = 0.01\ \muF and equal resistors

No cutoff frequency is given, so assume a half-power frequency of 1 kHz (the same steps hold for any frequency; only kfk_f changes).

From Table 1: T(s)=1s2+1.414s+1T(s) = \dfrac{1}{s^2 + 1.414s + 1}, so ωo=1\omega_o = 1, Q=0.7071Q = 0.7071.

Equal-element design (Design 1): take normalized R1=R2=1 ΩR_1 = R_2 = 1\ \Omega, C1=C2=1C_1 = C_2 = 1 F. Then ωo=1\omega_o = 1 rad/s and

1Q=1+1+(1−K)=3−K  ⇒  K=3−1Q\frac{1}{Q} = 1 + 1 + (1 - K) = 3 - K \;\Rightarrow\; K = 3 - \frac{1}{Q} K=3−1.414=1.586,RBRA=0.586K = 3 - 1.414 = 1.586, \qquad \frac{R_B}{R_A} = 0.586

Scaling (CC must become 0.01 μF):

kf=2π×1000=6283.19 rad/skm=Cnkf C=16283.19×10−8=15 915.5R1=R2=15.92 kΩ\begin{aligned} k_f &= 2\pi \times 1000 = 6283.19\ \text{rad/s} \\ k_m &= \frac{C_n}{k_f\,C} = \frac{1}{6283.19 \times 10^{-8}} = 15\,915.5 \\ R_1 = R_2 &= 15.92\ \text{k}\Omega \end{aligned}

With RA=10 kΩR_A = 10\ \text{k}\Omega: RB=5.86 kΩR_B = 5.86\ \text{k}\Omega.

ElementValue
R1=R2R_1 = R_215.92 kΩ
C1=C2C_1 = C_20.01 μF
RA,RBR_A, R_B10 kΩ, 5.86 kΩ

Answer: R1=R2=15.92 kΩR_1 = R_2 = 15.92\ \text{k}\Omega, C1=C2=0.01 μC_1 = C_2 = 0.01\ \muF, K=1.586K = 1.586 (RB=5.86 kΩR_B = 5.86\ \text{k}\Omega, RA=10 kΩR_A = 10\ \text{k}\Omega), fc=1f_c = 1 kHz. For another fcf_c, R=12πfc×0.01 μFR = \dfrac{1}{2\pi f_c \times 0.01\ \mu\text{F}} (for example 1.59 kΩ at 10 kHz).

  • 2081 Baisakh · 4+4 marks

Derive the transfer function of low pass sallen-key biquad filter. (Refer Table 1) The half power frequency should be 10 KHz. Make the largest capacitance 0.01μF and overall gain be 1.

Answer

Transfer function of the Sallen-Key low-pass biquad

The Sallen-Key low-pass biquad uses one op-amp wired as a non-inverting amplifier of gain K=1+RB/RAK = 1 + R_B/R_A, two resistors R1,R2R_1, R_2 in series, a capacitor C1C_1 fed back from the output to node A, and a grounded capacitor C2C_2 at node B.

              C1 (feedback)
        +-----||-------------+
        |                    |
Vin -R1-+-(A)- R2 -+-(B)--|+\ |
                   |      |  >+---- Vo
                  === C2 +|-/ |
                   |     |    |
                  GND    +-RB-+
                         |
                         RA
                         |
                        GND

Derivation (ideal op-amp, so Vo=KVBV_o = K V_B and no current enters the + input):

Node B: the current through R2R_2 flows into C2C_2:

VA−VBR2=sC2VB  ⇒  VA=VB(1+sR2C2)\frac{V_A - V_B}{R_2} = sC_2 V_B \;\Rightarrow\; V_A = V_B(1 + sR_2C_2)

Node A (KCL):

Vin−VAR1=VA−VBR2+sC1(VA−Vo)\frac{V_{in} - V_A}{R_1} = \frac{V_A - V_B}{R_2} + sC_1 (V_A - V_o)

Substituting VAV_A and VB=Vo/KV_B = V_o/K and simplifying:

T(s)=VoVin=KR1R2C1C2s2+s(1R1C1+1R2C1+1−KR2C2)+1R1R2C1C2T(s) = \frac{V_o}{V_{in}} = \frac{\dfrac{K}{R_1R_2C_1C_2}}{s^2 + s\left(\dfrac{1}{R_1C_1} + \dfrac{1}{R_2C_1} + \dfrac{1-K}{R_2C_2}\right) + \dfrac{1}{R_1R_2C_1C_2}}

Comparing with T(s)=Kωo2s2+(ωo/Q)s+ωo2T(s) = \dfrac{K\omega_o^2}{s^2 + (\omega_o/Q)s + \omega_o^2}:

ωo=1R1R2C1C2ωoQ=1R1C1+1R2C1+1−KR2C2\begin{aligned} \omega_o &= \frac{1}{\sqrt{R_1R_2C_1C_2}} \\ \frac{\omega_o}{Q} &= \frac{1}{R_1C_1} + \frac{1}{R_2C_1} + \frac{1-K}{R_2C_2} \end{aligned}

DC gain =K= K.

Design: fc=10f_c = 10 kHz, largest C=0.01 μC = 0.01\ \muF, overall gain 1

Assume a Butterworth response (Table 1): T(s)=1s2+2s+1T(s) = \dfrac{1}{s^2 + \sqrt2 s + 1}, so ωo=1\omega_o = 1 and Q=0.7071Q = 0.7071.

Gain 1 needs K=1K = 1 (RB=0R_B = 0, RAR_A open: a voltage follower). This is the unity-gain design (Design 2). Take R1=R2=1 ΩR_1 = R_2 = 1\ \Omega:

ωo2=1C1C2=1ωoQ=2C1+0=2  ⇒  C1=2Q=1.414 F,  C2=12Q=0.7071 F\begin{aligned} \omega_o^2 &= \frac{1}{C_1C_2} = 1 \\ \frac{\omega_o}{Q} &= \frac{2}{C_1} + 0 = \sqrt2 \end{aligned} \;\Rightarrow\; C_1 = 2Q = 1.414\ \text{F},\; C_2 = \frac{1}{2Q} = 0.7071\ \text{F}

The largest capacitor is C1C_1 (the feedback capacitor).

Scaling:

kf=2π×104=62 831.85km=1.41462 831.85×0.01×10−6=2250.8C1=0.01 μF,C2=0.7071kfkm=0.005 μFR1=R2=2250.8 Ω≈2.25 kΩ\begin{aligned} k_f &= 2\pi\times 10^4 = 62\,831.85 \\ k_m &= \frac{1.414}{62\,831.85 \times 0.01\times10^{-6}} = 2250.8 \\ C_1 &= 0.01\ \mu\text{F}, \quad C_2 = \frac{0.7071}{k_f k_m} = 0.005\ \mu\text{F} \\ R_1 = R_2 &= 2250.8\ \Omega \approx 2.25\ \text{k}\Omega \end{aligned}

Answer: R1=R2=2.25 kΩR_1 = R_2 = 2.25\ \text{k}\Omega, C1=0.01 μC_1 = 0.01\ \muF (output feedback), C2=5C_2 = 5 nF (to ground), op-amp as a voltage follower. DC gain = 1, fc=10f_c = 10 kHz, Q=0.707Q = 0.707.

  • 2081 Bhadra · 5+4 marks

Draw the circuit diagram of Sallen and Key LP biquad and derive its transfer function. Design a MFB LP biquad for the transfer function as T(s) = 5/(s² + 1.2s + 1).

Answer

Sallen-Key LP biquad and its transfer function

The Sallen-Key low-pass biquad uses one op-amp wired as a non-inverting amplifier of gain K=1+RB/RAK = 1 + R_B/R_A, two resistors R1,R2R_1, R_2 in series, a capacitor C1C_1 fed back from the output to node A, and a grounded capacitor C2C_2 at node B.

              C1 (feedback)
        +-----||-------------+
        |                    |
Vin -R1-+-(A)- R2 -+-(B)--|+\ |
                   |      |  >+---- Vo
                  === C2 +|-/ |
                   |     |    |
                  GND    +-RB-+
                         |
                         RA
                         |
                        GND

Derivation (ideal op-amp, so Vo=KVBV_o = K V_B and no current enters the + input):

Node B: the current through R2R_2 flows into C2C_2:

VA−VBR2=sC2VB  ⇒  VA=VB(1+sR2C2)\frac{V_A - V_B}{R_2} = sC_2 V_B \;\Rightarrow\; V_A = V_B(1 + sR_2C_2)

Node A (KCL):

Vin−VAR1=VA−VBR2+sC1(VA−Vo)\frac{V_{in} - V_A}{R_1} = \frac{V_A - V_B}{R_2} + sC_1 (V_A - V_o)

Substituting VAV_A and VB=Vo/KV_B = V_o/K and simplifying:

T(s)=VoVin=KR1R2C1C2s2+s(1R1C1+1R2C1+1−KR2C2)+1R1R2C1C2T(s) = \frac{V_o}{V_{in}} = \frac{\dfrac{K}{R_1R_2C_1C_2}}{s^2 + s\left(\dfrac{1}{R_1C_1} + \dfrac{1}{R_2C_1} + \dfrac{1-K}{R_2C_2}\right) + \dfrac{1}{R_1R_2C_1C_2}}

Comparing with T(s)=Kωo2s2+(ωo/Q)s+ωo2T(s) = \dfrac{K\omega_o^2}{s^2 + (\omega_o/Q)s + \omega_o^2}:

ωo=1R1R2C1C2ωoQ=1R1C1+1R2C1+1−KR2C2\begin{aligned} \omega_o &= \frac{1}{\sqrt{R_1R_2C_1C_2}} \\ \frac{\omega_o}{Q} &= \frac{1}{R_1C_1} + \frac{1}{R_2C_1} + \frac{1-K}{R_2C_2} \end{aligned}

DC gain =K= K.

MFB low-pass design for T(s)=5/(s2+1.2s+1)T(s) = 5/(s^2 + 1.2s + 1)

The multiple-feedback (MFB, Rauch) low-pass circuit uses an inverting op-amp: R1R_1 from VinV_{in} to node A, C1C_1 from A to ground, R3R_3 from A to VoV_o, R2R_2 from A to the inverting input, and C2C_2 from the inverting input to VoV_o.

              +-----R3-----------+
              |                  |
              |      +---||--+   |
              |      |   C2  |   |
Vin --R1--+--(A)--R2-+--|-\   |   |
          |             |  >--+---+-- Vo
         === C1    GND--|+/
          |
         GND

Its transfer function is

T(s)=−1R1R2C1C2s2+sC1(1R1+1R2+1R3)+1R2R3C1C2,∣HDC∣=R3R1T(s) = \frac{-\dfrac{1}{R_1R_2C_1C_2}}{s^2 + \dfrac{s}{C_1}\left(\dfrac1{R_1} + \dfrac1{R_2} + \dfrac1{R_3}\right) + \dfrac{1}{R_2R_3C_1C_2}}, \qquad |H_{DC}| = \frac{R_3}{R_1}

Given: ωo=1\omega_o = 1, ωo/Q=1.2\omega_o/Q = 1.2 (Q=0.833Q = 0.833), H=5H = 5.

For real resistors the capacitor ratio must satisfy C1/C2≥4Q2(1+H)=4(0.694)(6)=16.67C_1/C_2 \ge 4Q^2(1+H) = 4(0.694)(6) = 16.67. Take C2=1C_2 = 1 F and C1=16.67C_1 = 16.67 F (the minimum, which gives equal roots):

R2R3=1C1C2=0.06,R3=5R1116.67(1.2R1+1R2)=1.2  ⇒  100R2+1R2=20(10R2−1)2=0  ⇒  R2=0.1 Ω,  R3=0.6 Ω,  R1=0.12 Ω\begin{aligned} R_2R_3 &= \frac{1}{C_1C_2} = 0.06, \quad R_3 = 5R_1 \\ \frac{1}{16.67}\left(\frac{1.2}{R_1} + \frac{1}{R_2}\right) &= 1.2 \;\Rightarrow\; 100R_2 + \frac{1}{R_2} = 20 \\ (10R_2 - 1)^2 &= 0 \;\Rightarrow\; R_2 = 0.1\ \Omega,\; R_3 = 0.6\ \Omega,\; R_1 = 0.12\ \Omega \end{aligned}

(Here R1=R3/5=0.012/R2R_1 = R_3/5 = 0.012/R_2 was substituted.)

Check: 1R1R2C1C2=10.12×0.1×16.67=5\dfrac{1}{R_1R_2C_1C_2} = \dfrac{1}{0.12\times0.1\times16.67} = 5, 1C1(8.33+10+1.67)=1.2\dfrac{1}{C_1}(8.33 + 10 + 1.67) = 1.2, 1R2R3C1C2=1\dfrac{1}{R_2R_3C_1C_2} = 1. Correct.

Practical values: the given T(s)T(s) is normalized, so assume ωo=104\omega_o = 10^4 rad/s (kf=104k_f = 10^4) and km=104k_m = 10^4:

ElementNormalizedScaled
R1R_10.12 Ω1.2 kΩ
R2R_20.1 Ω1 kΩ
R3R_30.6 Ω6 kΩ
C1C_116.67 F166.7 nF
C2C_21 F10 nF

Answer: R1=0.12R_1 = 0.12, R2=0.1R_2 = 0.1, R3=0.6 ΩR_3 = 0.6\ \Omega, C1=16.67C_1 = 16.67, C2=1C_2 = 1 F (normalized). The gain is −5-5; the sign only adds a 180° phase shift.

  • 2082 Baisakh · 6 marks

Design a second order Butterworth low pass filter using a Sallen and Key Biquad circuit. Use design 2 method.

Answer

In Design 2 (unity-gain design) of the Sallen-Key low-pass biquad, the op-amp is a voltage follower (K=1K = 1) and the two resistors are equal; the capacitors are then chosen to set QQ.

              C1 (feedback)
        +-----||-------------+
        |                    |
Vin -R1-+-(A)- R2 -+-(B)--|+\ |
                   |      |  >+---- Vo
                  === C2 +|-/ |
                   |     |    |
                  GND    +-RB-+
                         |
                         RA
                         |
                        GND

(For K=1K = 1: RB=0R_B = 0 and RAR_A is removed.)

Transfer function with K = 1:

T(s)=1R1R2C1C2s2+s(1R1C1+1R2C1)+1R1R2C1C2T(s) = \frac{\dfrac{1}{R_1R_2C_1C_2}}{s^2 + s\left(\dfrac{1}{R_1C_1} + \dfrac{1}{R_2C_1}\right) + \dfrac{1}{R_1R_2C_1C_2}}

Normalized design (ωo=1\omega_o = 1): 2nd-order Butterworth T(s)=1s2+2s+1T(s) = \dfrac{1}{s^2 + \sqrt2 s + 1}, Q=0.7071Q = 0.7071. With R1=R2=1 ΩR_1 = R_2 = 1\ \Omega:

ωo2=1C1C2=1ωoQ=2C1=2⇒C1=2Q=1.414 F,C2=12Q=0.7071 F\begin{aligned} \omega_o^2 &= \frac{1}{C_1C_2} = 1 \\ \frac{\omega_o}{Q} &= \frac{2}{C_1} = \sqrt2 \\ \Rightarrow C_1 &= 2Q = 1.414\ \text{F}, \quad C_2 = \frac{1}{2Q} = 0.7071\ \text{F} \end{aligned}

Capacitor ratio C1/C2=4Q2=2C_1/C_2 = 4Q^2 = 2.

Denormalization: no frequency is given, so assume fc=1f_c = 1 kHz and make the largest capacitor C1=0.01 μC_1 = 0.01\ \muF:

kf=2π×1000=6283.19km=1.4146283.19×10−8=22 508R1=R2=22.5 kΩC1=0.01 μF,C2=0.70716283.19×22 508=5 nF\begin{aligned} k_f &= 2\pi\times1000 = 6283.19 \\ k_m &= \frac{1.414}{6283.19 \times 10^{-8}} = 22\,508 \\ R_1 = R_2 &= 22.5\ \text{k}\Omega \\ C_1 &= 0.01\ \mu\text{F}, \quad C_2 = \frac{0.7071}{6283.19 \times 22\,508} = 5\ \text{nF} \end{aligned}
ElementNormalizedFinal (fcf_c = 1 kHz)
R1=R2R_1 = R_21 Ω22.5 kΩ
C1C_1 (feedback)1.414 F0.01 μF
C2C_2 (to ground)0.7071 F5 nF
Gain KK11 (follower)

Answer: R1=R2=22.5 kΩR_1 = R_2 = 22.5\ \text{k}\Omega, C1=10C_1 = 10 nF, C2=5C_2 = 5 nF, unity-gain follower. This gives a Butterworth response with fc=1f_c = 1 kHz and DC gain 1.

Features of Design 2: unity gain, so it needs no gain resistors and the op-amp works as a follower (wide bandwidth). Gain sensitivity is low (SKQS^{Q}_{K} small), but the capacitor spread 4Q24Q^2 grows quickly at high QQ.

  • 2073 Chaitra · 4+4 marks

Derive the transfer function of Sallen and Key low pass Biquad. Using Sallen and Key circuit, design a lowpass filter having ωo of 1000 rad/sec, quality factor of 0.866 and gain of 2.

Answer

Transfer function of the Sallen-Key low-pass biquad

The Sallen-Key low-pass biquad uses one op-amp wired as a non-inverting amplifier of gain K=1+RB/RAK = 1 + R_B/R_A, two resistors R1,R2R_1, R_2 in series, a capacitor C1C_1 fed back from the output to node A, and a grounded capacitor C2C_2 at node B.

              C1 (feedback)
        +-----||-------------+
        |                    |
Vin -R1-+-(A)- R2 -+-(B)--|+\ |
                   |      |  >+---- Vo
                  === C2 +|-/ |
                   |     |    |
                  GND    +-RB-+
                         |
                         RA
                         |
                        GND

Derivation (ideal op-amp, so Vo=KVBV_o = K V_B and no current enters the + input):

Node B: the current through R2R_2 flows into C2C_2:

VA−VBR2=sC2VB  ⇒  VA=VB(1+sR2C2)\frac{V_A - V_B}{R_2} = sC_2 V_B \;\Rightarrow\; V_A = V_B(1 + sR_2C_2)

Node A (KCL):

Vin−VAR1=VA−VBR2+sC1(VA−Vo)\frac{V_{in} - V_A}{R_1} = \frac{V_A - V_B}{R_2} + sC_1 (V_A - V_o)

Substituting VAV_A and VB=Vo/KV_B = V_o/K and simplifying:

T(s)=VoVin=KR1R2C1C2s2+s(1R1C1+1R2C1+1−KR2C2)+1R1R2C1C2T(s) = \frac{V_o}{V_{in}} = \frac{\dfrac{K}{R_1R_2C_1C_2}}{s^2 + s\left(\dfrac{1}{R_1C_1} + \dfrac{1}{R_2C_1} + \dfrac{1-K}{R_2C_2}\right) + \dfrac{1}{R_1R_2C_1C_2}}

Comparing with T(s)=Kωo2s2+(ωo/Q)s+ωo2T(s) = \dfrac{K\omega_o^2}{s^2 + (\omega_o/Q)s + \omega_o^2}:

ωo=1R1R2C1C2ωoQ=1R1C1+1R2C1+1−KR2C2\begin{aligned} \omega_o &= \frac{1}{\sqrt{R_1R_2C_1C_2}} \\ \frac{\omega_o}{Q} &= \frac{1}{R_1C_1} + \frac{1}{R_2C_1} + \frac{1-K}{R_2C_2} \end{aligned}

DC gain =K= K.

Design: ωo=1000\omega_o = 1000 rad/s, Q=0.866Q = 0.866, gain 2

Equal-element design would give K=3−1/Q=3−1.1547=1.845K = 3 - 1/Q = 3 - 1.1547 = 1.845, which is not 2. So set K=2K = 2 (RB=RAR_B = R_A) and R1=R2=1R_1 = R_2 = 1, and find unequal capacitors (normalized ωo=1\omega_o = 1):

ωo2=1C1C2=1⇒C2=1C11Q=2C1+1−2C2=2C1−C1=1.1547C12+1.1547 C1−2=0C1=−1.1547+1.3333+82=0.9502 F,C2=1.0524 F\begin{aligned} \omega_o^2 &= \frac{1}{C_1C_2} = 1 \Rightarrow C_2 = \frac{1}{C_1} \\ \frac{1}{Q} &= \frac{2}{C_1} + \frac{1-2}{C_2} = \frac{2}{C_1} - C_1 = 1.1547 \\ C_1^2 &+ 1.1547\,C_1 - 2 = 0 \\ C_1 &= \frac{-1.1547 + \sqrt{1.3333 + 8}}{2} = 0.9502\ \text{F}, \quad C_2 = 1.0524\ \text{F} \end{aligned}

Check: 2/0.9502−1/1.0524=2.1048−0.9502=1.1547=1/Q2/0.9502 - 1/1.0524 = 2.1048 - 0.9502 = 1.1547 = 1/Q.

Denormalization: kf=1000k_f = 1000; choose km=104k_m = 10^4 so the capacitors are near 0.1 μF:

R1=R2=1×104=10 kΩC1=0.95021000×104=95.0 nFC2=1.05241000×104=105.2 nF\begin{aligned} R_1 = R_2 &= 1 \times 10^4 = 10\ \text{k}\Omega \\ C_1 &= \frac{0.9502}{1000\times10^4} = 95.0\ \text{nF} \\ C_2 &= \frac{1.0524}{1000\times10^4} = 105.2\ \text{nF} \end{aligned}

Gain K=1+RB/RA=2K = 1 + R_B/R_A = 2: take RA=RB=10 kΩR_A = R_B = 10\ \text{k}\Omega.

ElementValue
R1=R2R_1 = R_210 kΩ
C1C_1 (feedback)95.0 nF
C2C_2 (to ground)105.2 nF
RA=RBR_A = R_B10 kΩ

Answer: R1=R2=RA=RB=10 kΩR_1 = R_2 = R_A = R_B = 10\ \text{k}\Omega, C1=95.0C_1 = 95.0 nF, C2=105.2C_2 = 105.2 nF. This gives ωo=1000\omega_o = 1000 rad/s, Q=0.866Q = 0.866 and DC gain 2.

  • 2074 Asoj · 4+2+4 marks

Draw the circuit diagram of Sallen-Key lowpass biquad circuit and derive the transfer function. How can you obtain highpass filter from lowpass one? Design the second order lowpass Butterworth filter having half power frequency of 12 KHz using Sallen-Key biquad circuit. T2(s) = 1/(s² + √2 s + 1)

Answer

Sallen-Key low-pass circuit and transfer function

The Sallen-Key low-pass biquad uses one op-amp wired as a non-inverting amplifier of gain K=1+RB/RAK = 1 + R_B/R_A, two resistors R1,R2R_1, R_2 in series, a capacitor C1C_1 fed back from the output to node A, and a grounded capacitor C2C_2 at node B.

              C1 (feedback)
        +-----||-------------+
        |                    |
Vin -R1-+-(A)- R2 -+-(B)--|+\ |
                   |      |  >+---- Vo
                  === C2 +|-/ |
                   |     |    |
                  GND    +-RB-+
                         |
                         RA
                         |
                        GND

Derivation (ideal op-amp, so Vo=KVBV_o = K V_B and no current enters the + input):

Node B: the current through R2R_2 flows into C2C_2:

VA−VBR2=sC2VB  ⇒  VA=VB(1+sR2C2)\frac{V_A - V_B}{R_2} = sC_2 V_B \;\Rightarrow\; V_A = V_B(1 + sR_2C_2)

Node A (KCL):

Vin−VAR1=VA−VBR2+sC1(VA−Vo)\frac{V_{in} - V_A}{R_1} = \frac{V_A - V_B}{R_2} + sC_1 (V_A - V_o)

Substituting VAV_A and VB=Vo/KV_B = V_o/K and simplifying:

T(s)=VoVin=KR1R2C1C2s2+s(1R1C1+1R2C1+1−KR2C2)+1R1R2C1C2T(s) = \frac{V_o}{V_{in}} = \frac{\dfrac{K}{R_1R_2C_1C_2}}{s^2 + s\left(\dfrac{1}{R_1C_1} + \dfrac{1}{R_2C_1} + \dfrac{1-K}{R_2C_2}\right) + \dfrac{1}{R_1R_2C_1C_2}}

Comparing with T(s)=Kωo2s2+(ωo/Q)s+ωo2T(s) = \dfrac{K\omega_o^2}{s^2 + (\omega_o/Q)s + \omega_o^2}:

ωo=1R1R2C1C2ωoQ=1R1C1+1R2C1+1−KR2C2\begin{aligned} \omega_o &= \frac{1}{\sqrt{R_1R_2C_1C_2}} \\ \frac{\omega_o}{Q} &= \frac{1}{R_1C_1} + \frac{1}{R_2C_1} + \frac{1-K}{R_2C_2} \end{aligned}

DC gain =K= K.

Obtaining a high-pass filter from the low-pass one

Use the RC-CR transformation: replace every resistor RiR_i by a capacitor 1/Ri1/R_i and every capacitor CjC_j by a resistor 1/Cj1/C_j (normalized values). The op-amp gain resistors RA,RBR_A, R_B set only a ratio, so they stay unchanged. This replaces ss by 1/s1/s, so

THP(s)=Ks2s2+(ωo/Q)s+ωo2T_{HP}(s) = \frac{K s^2}{s^2 + (\omega_o/Q)s + \omega_o^2}

In the high-pass circuit, capacitors sit in the series positions and resistors in the feedback and grounded positions.

Design: Butterworth LPF at 12 kHz

T2(s)=1s2+2s+1T_2(s) = \dfrac{1}{s^2 + \sqrt2 s + 1}: ωo=1\omega_o = 1, Q=0.7071Q = 0.7071.

Equal-element design (Design 1): take normalized R1=R2=1 ΩR_1 = R_2 = 1\ \Omega, C1=C2=1C_1 = C_2 = 1 F. Then ωo=1\omega_o = 1 rad/s and

1Q=1+1+(1−K)=3−K  ⇒  K=3−1Q\frac{1}{Q} = 1 + 1 + (1 - K) = 3 - K \;\Rightarrow\; K = 3 - \frac{1}{Q} K=3−1.414=1.586,RB/RA=0.586K = 3 - 1.414 = 1.586, \quad R_B/R_A = 0.586

Scaling (choose C=0.01 μC = 0.01\ \muF):

kf=2π×12 000=75 398.2 rad/skm=175 398.2×10−8=1326.3R1=R2=1.326 kΩ\begin{aligned} k_f &= 2\pi \times 12\,000 = 75\,398.2\ \text{rad/s} \\ k_m &= \frac{1}{75\,398.2 \times 10^{-8}} = 1326.3 \\ R_1 = R_2 &= 1.326\ \text{k}\Omega \end{aligned}

RA=10 kΩR_A = 10\ \text{k}\Omega, RB=5.86 kΩR_B = 5.86\ \text{k}\Omega.

Answer: R1=R2=1.33 kΩR_1 = R_2 = 1.33\ \text{k}\Omega, C1=C2=0.01 μC_1 = C_2 = 0.01\ \muF, RA=10 kΩR_A = 10\ \text{k}\Omega, RB=5.86 kΩR_B = 5.86\ \text{k}\Omega; fc=12f_c = 12 kHz, DC gain 1.586.

  • 2081 Baisakh · 4+4 marks

Draw the circuit diagram of Sallen-Key lowpass biquad circuit and derive the transfer function. Realize the normalized transfer function of 1/(s²+s+1) using Sallen-Key biquad circuit. In your final design the half power frequency should be 1.8 kHz and all capacitances of 10nF.

Answer

Sallen-Key low-pass circuit and transfer function

The Sallen-Key low-pass biquad uses one op-amp wired as a non-inverting amplifier of gain K=1+RB/RAK = 1 + R_B/R_A, two resistors R1,R2R_1, R_2 in series, a capacitor C1C_1 fed back from the output to node A, and a grounded capacitor C2C_2 at node B.

              C1 (feedback)
        +-----||-------------+
        |                    |
Vin -R1-+-(A)- R2 -+-(B)--|+\ |
                   |      |  >+---- Vo
                  === C2 +|-/ |
                   |     |    |
                  GND    +-RB-+
                         |
                         RA
                         |
                        GND

Derivation (ideal op-amp, so Vo=KVBV_o = K V_B and no current enters the + input):

Node B: the current through R2R_2 flows into C2C_2:

VA−VBR2=sC2VB  ⇒  VA=VB(1+sR2C2)\frac{V_A - V_B}{R_2} = sC_2 V_B \;\Rightarrow\; V_A = V_B(1 + sR_2C_2)

Node A (KCL):

Vin−VAR1=VA−VBR2+sC1(VA−Vo)\frac{V_{in} - V_A}{R_1} = \frac{V_A - V_B}{R_2} + sC_1 (V_A - V_o)

Substituting VAV_A and VB=Vo/KV_B = V_o/K and simplifying:

T(s)=VoVin=KR1R2C1C2s2+s(1R1C1+1R2C1+1−KR2C2)+1R1R2C1C2T(s) = \frac{V_o}{V_{in}} = \frac{\dfrac{K}{R_1R_2C_1C_2}}{s^2 + s\left(\dfrac{1}{R_1C_1} + \dfrac{1}{R_2C_1} + \dfrac{1-K}{R_2C_2}\right) + \dfrac{1}{R_1R_2C_1C_2}}

Comparing with T(s)=Kωo2s2+(ωo/Q)s+ωo2T(s) = \dfrac{K\omega_o^2}{s^2 + (\omega_o/Q)s + \omega_o^2}:

ωo=1R1R2C1C2ωoQ=1R1C1+1R2C1+1−KR2C2\begin{aligned} \omega_o &= \frac{1}{\sqrt{R_1R_2C_1C_2}} \\ \frac{\omega_o}{Q} &= \frac{1}{R_1C_1} + \frac{1}{R_2C_1} + \frac{1-K}{R_2C_2} \end{aligned}

DC gain =K= K.

Realization of 1/(s2+s+1)1/(s^2 + s + 1) at 1.8 kHz with all C = 10 nF

Comparing: ωo=1\omega_o = 1, ωo/Q=1\omega_o/Q = 1, so Q=1Q = 1.

All capacitors are equal, so use the equal-element design (R1=R2=1R_1 = R_2 = 1, C1=C2=1C_1 = C_2 = 1):

K=3−1Q=3−1=2  ⇒  RB=RAK = 3 - \frac{1}{Q} = 3 - 1 = 2 \;\Rightarrow\; R_B = R_A

The half-power frequency is taken as the scaling frequency ωo\omega_o, as the question asks:

kf=2π×1800=11 309.7 rad/skm=111 309.7×10×10−9=8841.9R1=R2=8.84 kΩ\begin{aligned} k_f &= 2\pi \times 1800 = 11\,309.7\ \text{rad/s} \\ k_m &= \frac{1}{11\,309.7 \times 10\times10^{-9}} = 8841.9 \\ R_1 = R_2 &= 8.84\ \text{k}\Omega \end{aligned}

Take RA=RB=10 kΩR_A = R_B = 10\ \text{k}\Omega.

The circuit gain is 2, but T(s)T(s) has DC gain 1. To get unity gain, apply gain reduction with α=1/K=0.5\alpha = 1/K = 0.5:

R1a=R1α=17.68 kΩ,R1b=R11−α=17.68 kΩR_{1a} = \frac{R_1}{\alpha} = 17.68\ \text{k}\Omega, \qquad R_{1b} = \frac{R_1}{1-\alpha} = 17.68\ \text{k}\Omega
ElementValue
R1aR_{1a} (Vin to A)17.68 kΩ
R1bR_{1b} (A to ground)17.68 kΩ
R2R_28.84 kΩ
C1=C2C_1 = C_210 nF
RA=RBR_A = R_B10 kΩ

Answer: R1=R2=8.84 kΩR_1 = R_2 = 8.84\ \text{k}\Omega, C1=C2=10C_1 = C_2 = 10 nF, K=2K = 2. With R1R_1 split into two 17.68 kΩ resistors, the realized function is exactly ωo2s2+ωos+ωo2\dfrac{\omega_o^2}{s^2 + \omega_o s + \omega_o^2} with ωo=2π(1800)\omega_o = 2\pi(1800) rad/s.

  • 2070 Asar · 3+4+4 marks

What are advantages of active filter over passive filter? Draw the circuit diagram of Sallen Key lowpass filter and derive its transfer function. Design a second order Butterworth lowpass filter having half power frequency of 4 kHz using Sallen Key circuit. Your final circuit should have all capacitors of 0.01μF. Perform gain compensation if necessary.

Answer

Advantages of active filters over passive filters

  1. No inductors: inductors are bulky, heavy, lossy and cannot be integrated, especially at low frequencies. Active filters use only R, C and op-amps.
  2. Gain: they can give passband gain greater than 1; passive filters always attenuate.
  3. Isolation/buffering: the op-amp has high input and low output impedance, so stages can be cascaded without loading, and design becomes stage-by-stage.
  4. Easy tuning: ωo\omega_o, QQ and gain can often be adjusted independently with resistors.
  5. Small size, low cost and suitable for IC fabrication.

Sallen-Key low-pass circuit and transfer function

The Sallen-Key low-pass biquad uses one op-amp wired as a non-inverting amplifier of gain K=1+RB/RAK = 1 + R_B/R_A, two resistors R1,R2R_1, R_2 in series, a capacitor C1C_1 fed back from the output to node A, and a grounded capacitor C2C_2 at node B.

              C1 (feedback)
        +-----||-------------+
        |                    |
Vin -R1-+-(A)- R2 -+-(B)--|+\ |
                   |      |  >+---- Vo
                  === C2 +|-/ |
                   |     |    |
                  GND    +-RB-+
                         |
                         RA
                         |
                        GND

Derivation (ideal op-amp, so Vo=KVBV_o = K V_B and no current enters the + input):

Node B: the current through R2R_2 flows into C2C_2:

VA−VBR2=sC2VB  ⇒  VA=VB(1+sR2C2)\frac{V_A - V_B}{R_2} = sC_2 V_B \;\Rightarrow\; V_A = V_B(1 + sR_2C_2)

Node A (KCL):

Vin−VAR1=VA−VBR2+sC1(VA−Vo)\frac{V_{in} - V_A}{R_1} = \frac{V_A - V_B}{R_2} + sC_1 (V_A - V_o)

Substituting VAV_A and VB=Vo/KV_B = V_o/K and simplifying:

T(s)=VoVin=KR1R2C1C2s2+s(1R1C1+1R2C1+1−KR2C2)+1R1R2C1C2T(s) = \frac{V_o}{V_{in}} = \frac{\dfrac{K}{R_1R_2C_1C_2}}{s^2 + s\left(\dfrac{1}{R_1C_1} + \dfrac{1}{R_2C_1} + \dfrac{1-K}{R_2C_2}\right) + \dfrac{1}{R_1R_2C_1C_2}}

Comparing with T(s)=Kωo2s2+(ωo/Q)s+ωo2T(s) = \dfrac{K\omega_o^2}{s^2 + (\omega_o/Q)s + \omega_o^2}:

ωo=1R1R2C1C2ωoQ=1R1C1+1R2C1+1−KR2C2\begin{aligned} \omega_o &= \frac{1}{\sqrt{R_1R_2C_1C_2}} \\ \frac{\omega_o}{Q} &= \frac{1}{R_1C_1} + \frac{1}{R_2C_1} + \frac{1-K}{R_2C_2} \end{aligned}

DC gain =K= K.

Design: Butterworth LPF at 4 kHz, all C = 0.01 μF

T(s)=1s2+2s+1T(s) = \dfrac{1}{s^2 + \sqrt2 s + 1}, Q=0.7071Q = 0.7071. Equal-element design gives

K=3−2=1.586,RB/RA=0.586K = 3 - \sqrt2 = 1.586, \quad R_B/R_A = 0.586

Scaling:

kf=2π×4000=25 132.7km=125 132.7×10−8=3978.9R1=R2=3.98 kΩ\begin{aligned} k_f &= 2\pi\times4000 = 25\,132.7 \\ k_m &= \frac{1}{25\,132.7 \times 10^{-8}} = 3978.9 \\ R_1 = R_2 &= 3.98\ \text{k}\Omega \end{aligned}

Gain compensation: the circuit has gain 1.586, but the Butterworth function has gain 1. Use an input divider with α=1/K=0.6306\alpha = 1/K = 0.6306:

R1a=R1α=3978.90.6306=6.31 kΩR1b=R11−α=3978.90.3694=10.77 kΩ\begin{aligned} R_{1a} &= \frac{R_1}{\alpha} = \frac{3978.9}{0.6306} = 6.31\ \text{k}\Omega \\ R_{1b} &= \frac{R_1}{1-\alpha} = \frac{3978.9}{0.3694} = 10.77\ \text{k}\Omega \end{aligned}

R1a∥R1b=3.98 kΩ=R1R_{1a}\parallel R_{1b} = 3.98\ \text{k}\Omega = R_1, so ωo\omega_o and QQ are unchanged.

ElementValue
R1aR_{1a} (Vin to A)6.31 kΩ
R1bR_{1b} (A to ground)10.77 kΩ
R2R_23.98 kΩ
C1=C2C_1 = C_20.01 μF
RAR_A, RBR_B10 kΩ, 5.86 kΩ

Answer: R2=3.98 kΩR_2 = 3.98\ \text{k}\Omega, C1=C2=0.01 μC_1 = C_2 = 0.01\ \muF, RA=10 kΩR_A = 10\ \text{k}\Omega, RB=5.86 kΩR_B = 5.86\ \text{k}\Omega, with R1R_1 split into 6.31 kΩ and 10.77 kΩ. This gives fc=4f_c = 4 kHz and overall DC gain 1.

  • 2081 Bhadra · 2+4 marks

Why gain enhancement is needed in Sallen and Key biquad? Explain the gain enhancement in Sallen and Key low pass biquad.

Answer

Why gain enhancement is needed

In the Sallen-Key low-pass biquad the gain KK is not a free design parameter: it also sets QQ.

ωoQ=1R1C1+1R2C1+1−KR2C2\frac{\omega_o}{Q} = \frac{1}{R_1C_1} + \frac{1}{R_2C_1} + \frac{1-K}{R_2C_2}
  • Equal-element design: K=3−1/QK = 3 - 1/Q, so KK always lies between 1 and 3 (e.g. 1.586 for Butterworth).
  • Unity-gain design (Design 2): K=1K = 1.

Once QQ is chosen, the passband gain is fixed. If the specification needs a larger gain (say 10), the circuit cannot give it directly, so the gain must be enhanced without changing ωo\omega_o and QQ. (If the gain is too large, it is reduced with an input voltage divider instead.)

Gain enhancement in the Sallen-Key low-pass biquad

The idea is to let the op-amp amplify by a larger factor μ\mu while the feedback capacitor C1C_1 still sees only the voltage KVBK V_B that the design needs.

  1. Set the op-amp's non-inverting gain to μ=1+RB/RA\mu = 1 + R_B/R_A, larger than the design value KK.
  2. Connect a resistive divider RxR_x, RyR_y across the output. Return C1C_1 to the tap of this divider (not to VoV_o). The tap voltage is
Vt=βVo,β=RyRx+RyV_t = \beta V_o, \qquad \beta = \frac{R_y}{R_x + R_y}
  1. Choose β=K/μ\beta = K/\mu, so that Vt=βμVB=KVBV_t = \beta\mu V_B = K V_B.
               C1
        +------||-----+ tap (beta*Vo)
        |             |
Vin -R1-+- R2 -+------|+\       Rx
               |      |  >--+--/\/--+
              === C2 +|-/   |       |
               |     |      Vo     Ry
              GND  RA/RB           |
                   network        GND

Analysis: the node equations are the same as in the normal circuit, with VoV_o replaced by βVo=KVB\beta V_o = K V_B at C1C_1. So the denominator (and therefore ωo\omega_o and QQ) is unchanged:

VoVin=μ ωo2s2+(ωo/Q)s+ωo2,μ=Kβ\frac{V_o}{V_{in}} = \frac{\mu\,\omega_o^2}{s^2 + (\omega_o/Q)s + \omega_o^2}, \qquad \mu = \frac{K}{\beta}

The passband gain rises from KK to K/βK/\beta.

Design steps:

  1. Design the normal circuit for the required ωo\omega_o and QQ, which gives KK.
  2. Required gain HH: set μ=H\mu = H, i.e. RB/RA=H−1R_B/R_A = H - 1.
  3. Divider ratio β=K/H\beta = K/H.
  4. Keep Rx∥RyR_x \parallel R_y much smaller than the reactance 1/(ωoC1)1/(\omega_o C_1) so the divider is not loaded by C1C_1.

Example: Butterworth equal-element design (K=1.586K = 1.586) needing H=10H = 10: RB/RA=9R_B/R_A = 9 and β=0.1586\beta = 0.1586.

A simpler alternative is to cascade the biquad with a non-inverting amplifier of gain H/KH/K, at the cost of one more op-amp.

  • 2073 Chaitra · 4 marks

Explain RC-CR transformation with suitable examples.

Answer

The RC-CR transformation converts an active RC low-pass filter into a high-pass filter (and vice versa) by swapping resistors and capacitors.

Rule (normalized values):

  • Each resistor RiR_i becomes a capacitor Ci′=1/RiC_i' = 1/R_i.
  • Each capacitor CjC_j becomes a resistor Rj′=1/CjR_j' = 1/C_j.
  • Resistors that only set a dimensionless gain ratio (op-amp gain resistors RA,RBR_A, R_B) are not changed.

Why it works: the transfer function of an RC-op-amp circuit depends on the products sRCsRC. Swapping gives admittances sCi′=s/RisC_i' = s/R_i and 1/Rj′=Cj1/R_j' = C_j, i.e. every admittance is scaled by ss and ss is replaced by 1/s1/s. Ratios of admittances are unchanged except for s→1/ss \to 1/s, which is the LP-to-HP transformation:

THP(s)=TLP(1s)T_{HP}(s) = T_{LP}\left(\frac{1}{s}\right)

Poles keep the same ωo\omega_o and QQ.

Example 1: first-order RC low-pass

TLP=11+sRC  →  R→C, C→R    THP=sRC1+sRCT_{LP} = \frac{1}{1 + sRC} \;\xrightarrow{\;R\to C,\ C\to R\;}\; T_{HP} = \frac{sRC}{1 + sRC}

(the series R becomes a series C, the shunt C becomes a shunt R).

Example 2: Sallen-Key low-pass to high-pass

LP:  Vin-R1-+-R2-+-->(+)       C1 from node to Vo
            |    C2 to ground

HP:  Vin-C1'-+-C2'-+-->(+)     R1' from node to Vo
             |     R2' to ground
Kωo2s2+ωoQs+ωo2  ⇒  Ks2s2+ωoQs+ωo2\frac{K\omega_o^2}{s^2 + \frac{\omega_o}{Q}s + \omega_o^2} \;\Rightarrow\; \frac{K s^2}{s^2 + \frac{\omega_o}{Q}s + \omega_o^2}

With equal-element values (R=C=1R = C = 1, K=3−1/QK = 3 - 1/Q), the HP circuit also has C′=R′=1C' = R' = 1 and the same KK.

Example 3: a band-pass circuit maps into another band-pass circuit with the same centre frequency and QQ (since BP is unchanged under s→1/ss \to 1/s).

  • 2078 Bhadra · 1+4 marks

What is active filter. Design an active filter using non-inverting op-amp configuration with following transfer function. T(s) = (s+8)/(s+2)

Answer

Active filter

An active filter is a filter built from resistors, capacitors and active devices (op-amps or transistors) instead of inductors. The active device provides gain and isolation between stages.

Design of T(s)=(s+8)/(s+2)T(s) = (s+8)/(s+2)

Non-inverting configuration: Z1Z_1 from the inverting input to ground, Z2Z_2 from output to inverting input:

T(s)=1+Z2Z1T(s) = 1 + \frac{Z_2}{Z_1}

Here the zero (8) is larger than the pole (2), the high-frequency gain is 1 and the DC gain is 8/2=48/2 = 4. Use Z1=R1Z_1 = R_1 and Z2=R2∥C2Z_2 = R_2 \parallel C_2:

T(s)=1+R2R1(1+sR2C2)=s+R1+R2R1R2C2s+1R2C2\begin{aligned} T(s) &= 1 + \frac{R_2}{R_1(1 + sR_2C_2)} \\ &= \frac{s + \frac{R_1 + R_2}{R_1R_2C_2}}{s + \frac{1}{R_2C_2}} \end{aligned}
          +---R2---+
          |        |
          +---||---+
          |   C2   |
   +------+-|-\    |
   |        |  >---+---- Vo
  R1  Vin---|+/
   |
  GND

Matching coefficients:

1R2C2=21R2C2(1+R2R1)=8⇒1+R2R1=4⇒R2=3R1\begin{aligned} \frac{1}{R_2C_2} &= 2 \\ \frac{1}{R_2C_2}\left(1 + \frac{R_2}{R_1}\right) &= 8 \Rightarrow 1 + \frac{R_2}{R_1} = 4 \Rightarrow R_2 = 3R_1 \end{aligned}

Normalized: C2=1C_2 = 1 F, R2=0.5 ΩR_2 = 0.5\ \Omega, R1=0.1667 ΩR_1 = 0.1667\ \Omega.

Practical values (impedance scale only, since the poles are already in rad/s): choose C2=10 μC_2 = 10\ \muF:

R2=12×10×10−6=50 kΩ,R1=R23=16.67 kΩR_2 = \frac{1}{2 \times 10\times10^{-6}} = 50\ \text{k}\Omega, \qquad R_1 = \frac{R_2}{3} = 16.67\ \text{k}\Omega

Check: DC gain 1+R2/R1=4=8/21 + R_2/R_1 = 4 = 8/2; HF gain 1.

Answer: R1=16.67 kΩR_1 = 16.67\ \text{k}\Omega, R2=50 kΩR_2 = 50\ \text{k}\Omega, C2=10 μC_2 = 10\ \muF.

  • 2076 Asoj · 4+3 marks

What are the differences between active and passive filter? Design an active filter using non-inverting op-amp configuration with following transfer function. T(s) = (s+8)/(s+2)

Answer

Differences between active and passive filters

PointActive filterPassive filter
ElementsR, C and op-amps/transistorsR, L, C only
InductorsNot neededNeeded (bulky at low f)
GainCan be > 1Always ≤ 1 (loss)
Power supplyRequiredNot required
LoadingOp-amp buffers; easy cascadingStages load each other
Frequency rangeLimited by op-amp bandwidth (up to ~MHz)Works up to very high (RF) frequencies
Signal levelLimited by supply (saturation)Handles large voltage/current
NoiseOp-amp adds noiseLow noise (only R noise)
Size/ICSmall, can be integratedLarge; inductors cannot be integrated
SensitivityOften higherLow (doubly terminated ladders)

Design of T(s)=(s+8)/(s+2)T(s) = (s+8)/(s+2)

Non-inverting configuration: Z1Z_1 from the inverting input to ground, Z2Z_2 from output to inverting input:

T(s)=1+Z2Z1T(s) = 1 + \frac{Z_2}{Z_1}

Zero 8 > pole 2, high-frequency gain 1, DC gain 4. Use Z1=R1Z_1 = R_1, Z2=R2∥C2Z_2 = R_2 \parallel C_2:

T(s)=1+R2R1(1+sR2C2)=s+1R2C2(1+R2R1)s+1R2C2T(s) = 1 + \frac{R_2}{R_1(1 + sR_2C_2)} = \frac{s + \frac{1}{R_2C_2}\left(1+\frac{R_2}{R_1}\right)}{s + \frac{1}{R_2C_2}}
          +---R2---+
          |        |
          +---||---+
          |   C2   |
   +------+-|-\    |
   |        |  >---+---- Vo
  R1  Vin---|+/
   |
  GND

Matching: 1R2C2=2\dfrac{1}{R_2C_2} = 2 and 1+R2R1=82=41 + \dfrac{R_2}{R_1} = \dfrac{8}{2} = 4, so R2=3R1R_2 = 3R_1.

Normalized: C2=1C_2 = 1 F, R2=0.5 ΩR_2 = 0.5\ \Omega, R1=0.1667 ΩR_1 = 0.1667\ \Omega. With C2=10 μC_2 = 10\ \muF: R2=50 kΩR_2 = 50\ \text{k}\Omega, R1=16.67 kΩR_1 = 16.67\ \text{k}\Omega.

Answer: R1=16.67 kΩR_1 = 16.67\ \text{k}\Omega, R2=50 kΩR_2 = 50\ \text{k}\Omega, C2=10 μC_2 = 10\ \muF (DC gain 4, HF gain 1).

  • 2080 Bhadra · 2+3 marks

Differentiate active and passive filter. Realize the following transfer function using non-inverting op-amp configuration. T(s) = 4(s+2)/(s+1)

Answer

Active vs passive filters

PointActivePassive
ElementsR, C, op-ampR, L, C
GainCan exceed 1≤ 1
Power supplyNeededNot needed
InductorsAvoidedRequired
Frequency rangeLow to medium (op-amp limited)Up to RF
CascadingEasy (buffered)Loading problems

Realization of T(s)=4(s+2)/(s+1)T(s) = 4(s+2)/(s+1)

Gains: HF gain = 4, DC gain = 4×2/1=84 \times 2/1 = 8. The simple R∥CR \parallel C feedback gives HF gain 1 only, so add a series resistor RaR_a in the feedback path: Z1=R1Z_1 = R_1, Z2=Ra+(Rb∥C)Z_2 = R_a + (R_b \parallel C).

T(s)=1+1R1(Ra+Rb1+sRbC)=R1+RaR1⋅s+1RbC(1+RbR1+Ra)s+1RbC\begin{aligned} T(s) &= 1 + \frac{1}{R_1}\left(R_a + \frac{R_b}{1 + sR_bC}\right) \\ &= \frac{R_1 + R_a}{R_1}\cdot\frac{s + \frac{1}{R_bC}\left(1 + \frac{R_b}{R_1 + R_a}\right)}{s + \frac{1}{R_bC}} \end{aligned}
         +--Ra--+--Rb--+
         |      |      |
         |      +--||--+
         |         C   |
   +-----+-|-\         |
   |       |  >--------+--- Vo
  R1 Vin---|+/
   |
  GND

Matching:

1+RaR1=4⇒Ra=3R11RbC=11+RbR1+Ra=2⇒Rb=4R1\begin{aligned} 1 + \frac{R_a}{R_1} &= 4 \Rightarrow R_a = 3R_1 \\ \frac{1}{R_bC} &= 1 \\ 1 + \frac{R_b}{R_1 + R_a} &= 2 \Rightarrow R_b = 4R_1 \end{aligned}

Normalized (C=1C = 1 F): Rb=1 ΩR_b = 1\ \Omega, R1=0.25 ΩR_1 = 0.25\ \Omega, Ra=0.75 ΩR_a = 0.75\ \Omega.

Check: DC gain =1+(Ra+Rb)/R1=1+1.75/0.25=8= 1 + (R_a + R_b)/R_1 = 1 + 1.75/0.25 = 8. Correct.

Practical values (impedance scale km=105k_m = 10^5): R1=25 kΩR_1 = 25\ \text{k}\Omega, Ra=75 kΩR_a = 75\ \text{k}\Omega, Rb=100 kΩR_b = 100\ \text{k}\Omega, C=1/km=10 μC = 1/k_m = 10\ \muF.

Answer: R1=25 kΩR_1 = 25\ \text{k}\Omega, Ra=75 kΩR_a = 75\ \text{k}\Omega, Rb=100 kΩR_b = 100\ \text{k}\Omega, C=10 μC = 10\ \muF.

  • 2083 Baisakh · 4 marks

Realize an active filter using non-inverting op-amp configuration with zero at 8, pole at 4 and DC gain of 2.

Answer

The required function (zero at s=−8s=-8, pole at s=−4s=-4) is

T(s)=Ks+8s+4,T(0)=K⋅84=2⇒K=1T(s) = K\frac{s+8}{s+4}, \qquad T(0) = K\cdot\frac{8}{4} = 2 \Rightarrow K = 1

So T(s)=s+8s+4T(s) = \dfrac{s+8}{s+4}: DC gain 2, HF gain 1.

Non-inverting configuration: Z1Z_1 from the inverting input to ground, Z2Z_2 from output to inverting input:

T(s)=1+Z2Z1T(s) = 1 + \frac{Z_2}{Z_1}

Use Z1=R1Z_1 = R_1 and Z2=R2∥C2Z_2 = R_2 \parallel C_2:

T(s)=1+R2R1(1+sR2C2)=s+1R2C2(1+R2R1)s+1R2C2T(s) = 1 + \frac{R_2}{R_1(1+sR_2C_2)} = \frac{s + \frac{1}{R_2C_2}\left(1 + \frac{R_2}{R_1}\right)}{s + \frac{1}{R_2C_2}}
          +---R2---+
          |        |
          +---||---+
          |   C2   |
   +------+-|-\    |
   |        |  >---+---- Vo
  R1  Vin---|+/
   |
  GND

Matching:

1R2C2=41+R2R1=84=2⇒R1=R2\begin{aligned} \frac{1}{R_2C_2} &= 4 \\ 1 + \frac{R_2}{R_1} &= \frac{8}{4} = 2 \Rightarrow R_1 = R_2 \end{aligned}

Normalized: C2=1C_2 = 1 F, R1=R2=0.25 ΩR_1 = R_2 = 0.25\ \Omega.

Practical values: choose C2=10 μC_2 = 10\ \muF: R2=14×10−5=25 kΩ=R1R_2 = \dfrac{1}{4 \times 10^{-5}} = 25\ \text{k}\Omega = R_1.

Answer: R1=R2=25 kΩR_1 = R_2 = 25\ \text{k}\Omega, C2=10 μC_2 = 10\ \muF; DC gain 2, HF gain 1, zero at −8, pole at −4.

  • 2081 Bhadra · 5 marks

Realize a system using non-inverting op-amp configuration with zero at -5 and pole at -3 and having high frequency gain of 2.

Answer

Required function: zero at s=−5s = -5, pole at s=−3s = -3, high-frequency gain 2:

T(s)=2 s+5s+3T(s) = 2\,\frac{s+5}{s+3}

HF gain = 2, DC gain = 2×5/3=3.3332 \times 5/3 = 3.333.

Non-inverting configuration: Z1Z_1 from the inverting input to ground, Z2Z_2 from output to inverting input:

T(s)=1+Z2Z1T(s) = 1 + \frac{Z_2}{Z_1}

Since the zero is larger than the pole and the HF gain is above 1, use Z1=R1Z_1 = R_1 and Z2=Ra+(Rb∥C)Z_2 = R_a + (R_b \parallel C):

T(s)=1+1R1(Ra+Rb1+sRbC)=R1+RaR1⋅s+1RbC(1+RbR1+Ra)s+1RbC\begin{aligned} T(s) &= 1 + \frac{1}{R_1}\left(R_a + \frac{R_b}{1+sR_bC}\right) \\ &= \frac{R_1 + R_a}{R_1}\cdot\frac{s + \frac{1}{R_bC}\left(1 + \frac{R_b}{R_1+R_a}\right)}{s + \frac{1}{R_bC}} \end{aligned}
         +--Ra--+--Rb--+
         |      |      |
         |      +--||--+
         |         C   |
   +-----+-|-\         |
   |       |  >--------+--- Vo
  R1 Vin---|+/
   |
  GND

Matching:

1+RaR1=2⇒Ra=R11RbC=33(1+Rb2R1)=5⇒Rb=43R1\begin{aligned} 1 + \frac{R_a}{R_1} &= 2 \Rightarrow R_a = R_1 \\ \frac{1}{R_bC} &= 3 \\ 3\left(1 + \frac{R_b}{2R_1}\right) &= 5 \Rightarrow R_b = \frac{4}{3}R_1 \end{aligned}

Normalized (C=1C = 1 F): Rb=0.3333 ΩR_b = 0.3333\ \Omega, R1=Ra=0.25 ΩR_1 = R_a = 0.25\ \Omega.

Check: DC gain =1+Ra+RbR1=1+0.58330.25=3.333=2×53= 1 + \dfrac{R_a + R_b}{R_1} = 1 + \dfrac{0.5833}{0.25} = 3.333 = 2\times\frac53. Correct.

Practical values (km=105k_m = 10^5): R1=Ra=25 kΩR_1 = R_a = 25\ \text{k}\Omega, Rb=33.3 kΩR_b = 33.3\ \text{k}\Omega, C=10 μC = 10\ \muF.

Answer: R1=Ra=25 kΩR_1 = R_a = 25\ \text{k}\Omega, Rb=33.3 kΩR_b = 33.3\ \text{k}\Omega, C=10 μC = 10\ \muF.

  • 2079 Bhadra · 5 marks

Realize an active filter using non-inverting op-amp configuration with a zero at s = -4 and a pole at s = -8 having high frequency gain of k = 2.

Answer

Required function: zero at s=−4s=-4, pole at s=−8s=-8, HF gain 2:

T(s)=2 s+4s+8T(s) = 2\,\frac{s+4}{s+8}

DC gain =2×4/8=1= 2 \times 4/8 = 1. The zero is smaller than the pole (a lag-type network), with DC gain 1 and HF gain 2.

Non-inverting configuration: Z1Z_1 from the inverting input to ground, Z2Z_2 from output to inverting input:

T(s)=1+Z2Z1T(s) = 1 + \frac{Z_2}{Z_1}

Use Z2=R2Z_2 = R_2 and Z1=R1+1sC1Z_1 = R_1 + \dfrac{1}{sC_1} (series RC to ground):

T(s)=1+sR2C11+sR1C1=1+s(R1+R2)C11+sR1C1=R1+R2R1⋅s+1(R1+R2)C1s+1R1C1\begin{aligned} T(s) &= 1 + \frac{sR_2C_1}{1 + sR_1C_1} = \frac{1 + s(R_1+R_2)C_1}{1 + sR_1C_1} \\ &= \frac{R_1 + R_2}{R_1}\cdot\frac{s + \frac{1}{(R_1+R_2)C_1}}{s + \frac{1}{R_1C_1}} \end{aligned}
              +---R2---+
              |        |
   +----------+-|-\    |
   |            |  >---+--- Vo
  R1    Vin-----|+/
   |
  === C1
   |
  GND

Matching:

1R1C1=81(R1+R2)C1=4⇒R1+R2=2R1⇒R2=R1HF gain=R1+R2R1=2  (satisfied)\begin{aligned} \frac{1}{R_1C_1} &= 8 \\ \frac{1}{(R_1 + R_2)C_1} &= 4 \Rightarrow R_1 + R_2 = 2R_1 \Rightarrow R_2 = R_1 \\ \text{HF gain} &= \frac{R_1+R_2}{R_1} = 2 \;(\text{satisfied}) \end{aligned}

Normalized (C1=1C_1 = 1 F): R1=R2=0.125 ΩR_1 = R_2 = 0.125\ \Omega.

Practical values: choose C1=10 μC_1 = 10\ \muF: R1=18×10−5=12.5 kΩR_1 = \dfrac{1}{8 \times 10^{-5}} = 12.5\ \text{k}\Omega, R2=12.5 kΩR_2 = 12.5\ \text{k}\Omega.

Answer: R1=R2=12.5 kΩR_1 = R_2 = 12.5\ \text{k}\Omega, C1=10 μC_1 = 10\ \muF; T(s)=2(s+4)/(s+8)T(s) = 2(s+4)/(s+8).

  • 2071 Chaitra · 3 marks

Realize a system using inverting op-amp configuration with zero at s = -2 and pole at s = -5 and having high frequency gain of 2.

Answer

Required function: zero at s=−2s=-2, pole at s=−5s=-5, HF gain 2:

T(s)=2 s+2s+5(DC gain 0.8)T(s) = 2\,\frac{s+2}{s+5} \quad(\text{DC gain } 0.8)

Inverting configuration: Z1Z_1 from the input to the inverting input, Z2Z_2 in feedback:

T(s)=−Z2Z1=−Y1Y2T(s) = -\frac{Z_2}{Z_1} = -\frac{Y_1}{Y_2}

With Y1=1R1+sC1Y_1 = \dfrac{1}{R_1} + sC_1 (parallel R1C1R_1C_1) and Y2=1R2+sC2Y_2 = \dfrac{1}{R_2} + sC_2 (parallel R2C2R_2C_2):

T(s)=−C1C2⋅s+1R1C1s+1R2C2T(s) = -\frac{C_1}{C_2}\cdot\frac{s + \frac{1}{R_1C_1}}{s + \frac{1}{R_2C_2}}
              +---R2---+
              |        |
              +---||---+
       R1     |   C2   |
  +--/\/\--+  |        |
Vin        +--+-|-\    |
  +---||---+    |  >---+--- Vo
       C1   GND-|+/

Matching:

C1C2=21R1C1=21R2C2=5\begin{aligned} \frac{C_1}{C_2} &= 2 \\ \frac{1}{R_1C_1} &= 2 \\ \frac{1}{R_2C_2} &= 5 \end{aligned}

Normalized: C2=1C_2 = 1 F, C1=2C_1 = 2 F, R1=12×2=0.25 ΩR_1 = \dfrac{1}{2\times2} = 0.25\ \Omega, R2=0.2 ΩR_2 = 0.2\ \Omega.

Practical values (impedance scale km=105k_m = 10^5, C→C/kmC \to C/k_m):

ElementNormalizedFinal
R1R_10.25 Ω25 kΩ
C1C_12 F20 μF
R2R_20.2 Ω20 kΩ
C2C_21 F10 μF

Check: DC gain =R2/R1=0.8=2×2/5= R_2/R_1 = 0.8 = 2 \times 2/5; HF gain =C1/C2=2= C_1/C_2 = 2.

Answer: R1=25 kΩR_1 = 25\ \text{k}\Omega, C1=20 μC_1 = 20\ \muF, R2=20 kΩR_2 = 20\ \text{k}\Omega, C2=10 μC_2 = 10\ \muF, realizing −2(s+2)/(s+5)-2(s+2)/(s+5). The minus sign is the 180° phase inversion of this configuration; a unity-gain inverter can follow if a positive sign is needed.

  • 2069 Chaitra · 4 marks

Design the following transfer function using inverting op-amp configuration. T(s) = 7(s+400)/(s+200). You are not allowed to use inductors in the design.

Answer

Given T(s)=7s+400s+200T(s) = 7\dfrac{s+400}{s+200}: HF gain 7, DC gain 14, zero at −400, pole at −200. Only R, C and op-amps are used (no inductors).

Inverting configuration: Z1Z_1 from the input to the inverting input, Z2Z_2 in feedback:

T(s)=−Z2Z1=−Y1Y2T(s) = -\frac{Z_2}{Z_1} = -\frac{Y_1}{Y_2}

With Y1=1R1+sC1Y_1 = \dfrac{1}{R_1} + sC_1 (parallel R1C1R_1C_1) and Y2=1R2+sC2Y_2 = \dfrac{1}{R_2} + sC_2 (parallel R2C2R_2C_2):

T(s)=−C1C2⋅s+1R1C1s+1R2C2T(s) = -\frac{C_1}{C_2}\cdot\frac{s + \frac{1}{R_1C_1}}{s + \frac{1}{R_2C_2}}
              +---R2---+
              |        |
              +---||---+
       R1     |   C2   |
  +--/\/\--+  |        |
Vin        +--+-|-\    |
  +---||---+    |  >---+--- Vo
       C1   GND-|+/

Matching:

C1C2=71R1C1=4001R2C2=200\begin{aligned} \frac{C_1}{C_2} &= 7 \\ \frac{1}{R_1C_1} &= 400 \\ \frac{1}{R_2C_2} &= 200 \end{aligned}

Choose C2=0.1 μC_2 = 0.1\ \muF, so C1=0.7 μC_1 = 0.7\ \muF:

R1=1400×0.7×10−6=3.571 kΩR2=1200×0.1×10−6=50 kΩ\begin{aligned} R_1 &= \frac{1}{400 \times 0.7\times10^{-6}} = 3.571\ \text{k}\Omega \\ R_2 &= \frac{1}{200 \times 0.1\times10^{-6}} = 50\ \text{k}\Omega \end{aligned}

Check: DC gain =R2/R1=50/3.571=14=7×400/200= R_2/R_1 = 50/3.571 = 14 = 7 \times 400/200. Correct.

ElementValue
R1R_13.57 kΩ
C1C_10.7 μF
R2R_250 kΩ
C2C_20.1 μF

Answer: R1=3.57 kΩ∥C1=0.7 μR_1 = 3.57\ \text{k}\Omega \parallel C_1 = 0.7\ \muF at the input, R2=50 kΩ∥C2=0.1 μR_2 = 50\ \text{k}\Omega \parallel C_2 = 0.1\ \muF in feedback. The circuit gives −7(s+400)/(s+200)-7(s+400)/(s+200); add a unity-gain inverting amplifier (two equal resistors) if the positive sign is required.

  • 2080 Bhadra · 4 marks

Design the following transfer function using non-inverting op-amp configuration T(s) = 4(s+200)/(s+100)

Answer

Given T(s)=4s+200s+100T(s) = 4\dfrac{s+200}{s+100}: HF gain 4, DC gain 4×2=84\times2 = 8, zero at −200, pole at −100.

Non-inverting configuration: Z1Z_1 from the inverting input to ground, Z2Z_2 from output to inverting input:

T(s)=1+Z2Z1T(s) = 1 + \frac{Z_2}{Z_1}

Because the HF gain is greater than 1, use Z1=R1Z_1 = R_1 and Z2=Ra+(Rb∥C)Z_2 = R_a + (R_b \parallel C):

T(s)=R1+RaR1⋅s+1RbC(1+RbR1+Ra)s+1RbCT(s) = \frac{R_1 + R_a}{R_1}\cdot\frac{s + \frac{1}{R_bC}\left(1 + \frac{R_b}{R_1+R_a}\right)}{s + \frac{1}{R_bC}}
         +--Ra--+--Rb--+
         |      |      |
         |      +--||--+
         |         C   |
   +-----+-|-\         |
   |       |  >--------+--- Vo
  R1 Vin---|+/
   |
  GND

Matching:

1+RaR1=4⇒Ra=3R11RbC=100100(1+Rb4R1)=200⇒Rb=4R1\begin{aligned} 1 + \frac{R_a}{R_1} &= 4 \Rightarrow R_a = 3R_1 \\ \frac{1}{R_bC} &= 100 \\ 100\left(1 + \frac{R_b}{4R_1}\right) &= 200 \Rightarrow R_b = 4R_1 \end{aligned}

Choose C=1 μC = 1\ \muF:

Rb=1100×10−6=10 kΩ,R1=2.5 kΩ,Ra=7.5 kΩR_b = \frac{1}{100 \times 10^{-6}} = 10\ \text{k}\Omega,\quad R_1 = 2.5\ \text{k}\Omega,\quad R_a = 7.5\ \text{k}\Omega

Check: DC gain =1+(7.5+10)/2.5=8= 1 + (7.5 + 10)/2.5 = 8. Correct.

Answer: R1=2.5 kΩR_1 = 2.5\ \text{k}\Omega, Ra=7.5 kΩR_a = 7.5\ \text{k}\Omega, Rb=10 kΩR_b = 10\ \text{k}\Omega, C=1 μC = 1\ \muF.

  • 2080 Baisakh · 5 marks

Design a first order filter having a pole at -100 and a zero at -1000 with DC gain of 10 using non-inverting op-amp configuration.

Answer

Required function: pole at s=−100s=-100, zero at s=−1000s=-1000:

T(s)=Ks+1000s+100,T(0)=10K=10⇒K=1T(s) = K\frac{s+1000}{s+100}, \qquad T(0) = 10K = 10 \Rightarrow K = 1

So T(s)=s+1000s+100T(s) = \dfrac{s + 1000}{s + 100}: DC gain 10, HF gain 1.

Non-inverting configuration: Z1Z_1 from the inverting input to ground, Z2Z_2 from output to inverting input:

T(s)=1+Z2Z1T(s) = 1 + \frac{Z_2}{Z_1}

Use Z1=R1Z_1 = R_1 and Z2=R2∥C2Z_2 = R_2 \parallel C_2:

T(s)=s+1R2C2(1+R2R1)s+1R2C2T(s) = \frac{s + \frac{1}{R_2C_2}\left(1 + \frac{R_2}{R_1}\right)}{s + \frac{1}{R_2C_2}}
          +---R2---+
          |        |
          +---||---+
          |   C2   |
   +------+-|-\    |
   |        |  >---+---- Vo
  R1  Vin---|+/
   |
  GND

Matching:

1R2C2=1001+R2R1=1000100=10⇒R2=9R1\begin{aligned} \frac{1}{R_2C_2} &= 100 \\ 1 + \frac{R_2}{R_1} &= \frac{1000}{100} = 10 \Rightarrow R_2 = 9R_1 \end{aligned}

Choose C2=1 μC_2 = 1\ \muF:

R2=1100×10−6=10 kΩ,R1=109=1.111 kΩR_2 = \frac{1}{100\times10^{-6}} = 10\ \text{k}\Omega, \qquad R_1 = \frac{10}{9} = 1.111\ \text{k}\Omega

Answer: R1=1.11 kΩR_1 = 1.11\ \text{k}\Omega, R2=10 kΩR_2 = 10\ \text{k}\Omega, C2=1 μC_2 = 1\ \muF. DC gain =1+R2/R1=10= 1 + R_2/R_1 = 10, HF gain 1.

  • 2076 Chaitra · 3+3 marks

What are the advantages of active filter over passive filter? Realize an active filter having a pole at 100 and a zero at 1000 with a dc gain of 5.

Answer

Advantages of active filters over passive filters

  1. No inductors: avoids bulky, lossy, non-integrable inductors, which matters most at low (audio) frequencies.
  2. Gain: passband gain can exceed 1.
  3. No loading: high input and low output impedance allow cascading of independent sections.
  4. Easy tuning: ωo\omega_o, QQ and gain can be set by resistors.
  5. Small, light and cheap, and suitable for IC fabrication.

Realization: pole at −100, zero at −1000, DC gain 5

T(s)=Ks+1000s+100,T(0)=10K=5⇒K=0.5T(s) = K\frac{s + 1000}{s + 100}, \qquad T(0) = 10K = 5 \Rightarrow K = 0.5

So the HF gain is 0.5 and the DC gain is 5. A non-inverting stage cannot give a gain below 1, so use the inverting configuration with parallel RC branches:

T(s)=−Y1Y2=−C1C2⋅s+1R1C1s+1R2C2T(s) = -\frac{Y_1}{Y_2} = -\frac{C_1}{C_2}\cdot\frac{s + \frac{1}{R_1C_1}}{s + \frac{1}{R_2C_2}}
              +---R2---+
              +---||---+
       R1     |   C2   |
  +--/\/\--+  |        |
Vin        +--+-|-\    |
  +---||---+    |  >---+--- Vo
       C1   GND-|+/

Matching:

C1C2=0.5,1R1C1=1000,1R2C2=100\frac{C_1}{C_2} = 0.5,\qquad \frac{1}{R_1C_1} = 1000,\qquad \frac{1}{R_2C_2} = 100

Choose C2=1 μC_2 = 1\ \muF, so C1=0.5 μC_1 = 0.5\ \muF:

R1=11000×0.5×10−6=2 kΩ,R2=1100×10−6=10 kΩR_1 = \frac{1}{1000\times0.5\times10^{-6}} = 2\ \text{k}\Omega, \qquad R_2 = \frac{1}{100\times10^{-6}} = 10\ \text{k}\Omega

Check: DC gain =R2/R1=5= R_2/R_1 = 5. Correct.

Answer: R1=2 kΩR_1 = 2\ \text{k}\Omega, C1=0.5 μC_1 = 0.5\ \muF, R2=10 kΩR_2 = 10\ \text{k}\Omega, C2=1 μC_2 = 1\ \muF, realizing −0.5(s+1000)/(s+100)-0.5(s+1000)/(s+100) (|DC gain| = 5). The sign can be removed with a unity-gain inverter.

  • 2081 Baisakh · 2+5 marks

What are the advantages of active filters over passive filters? Realize a bilinear transfer function with a zero at 800, a pole at 400 and dc gain of 4 using non-inverting op-amp configuration.

Answer

Advantages of active filters over passive filters

  1. No inductors, so they are small, light and cheap, and work well at low frequencies.
  2. Gain greater than 1 is possible.
  3. High input and low output impedance, so sections can be cascaded without loading.
  4. ωo\omega_o, QQ and gain are easy to tune with resistors.
  5. Suitable for integrated-circuit fabrication.

Bilinear function: zero at −800, pole at −400, DC gain 4

T(s)=Ks+800s+400,T(0)=2K=4⇒K=2T(s) = K\frac{s + 800}{s + 400}, \qquad T(0) = 2K = 4 \Rightarrow K = 2

So HF gain = 2 and DC gain = 4.

Non-inverting configuration: T(s)=1+Z2/Z1T(s) = 1 + Z_2/Z_1. Since the HF gain is above 1, use Z1=R1Z_1 = R_1 and Z2=Ra+(Rb∥C)Z_2 = R_a + (R_b \parallel C):

T(s)=R1+RaR1⋅s+1RbC(1+RbR1+Ra)s+1RbCT(s) = \frac{R_1 + R_a}{R_1}\cdot\frac{s + \frac{1}{R_bC}\left(1 + \frac{R_b}{R_1 + R_a}\right)}{s + \frac{1}{R_bC}}
         +--Ra--+--Rb--+
         |      |      |
         |      +--||--+
         |         C   |
   +-----+-|-\         |
   |       |  >--------+--- Vo
  R1 Vin---|+/
   |
  GND

Matching:

1+RaR1=2⇒Ra=R11RbC=400400(1+Rb2R1)=800⇒Rb=2R1\begin{aligned} 1 + \frac{R_a}{R_1} &= 2 \Rightarrow R_a = R_1 \\ \frac{1}{R_bC} &= 400 \\ 400\left(1 + \frac{R_b}{2R_1}\right) &= 800 \Rightarrow R_b = 2R_1 \end{aligned}

Choose C=0.1 μC = 0.1\ \muF:

Rb=1400×0.1×10−6=25 kΩ,R1=Ra=12.5 kΩR_b = \frac{1}{400 \times 0.1\times10^{-6}} = 25\ \text{k}\Omega, \qquad R_1 = R_a = 12.5\ \text{k}\Omega

Check: DC gain =1+Ra+RbR1=1+37.512.5=4= 1 + \dfrac{R_a + R_b}{R_1} = 1 + \dfrac{37.5}{12.5} = 4. Correct.

Answer: R1=Ra=12.5 kΩR_1 = R_a = 12.5\ \text{k}\Omega, Rb=25 kΩR_b = 25\ \text{k}\Omega, C=0.1 μC = 0.1\ \muF.

  • 2079 Baisakh · 5 marks

What are the merits and demerits of active filter as compared with passive filter? Explain.

Answer

An active filter uses R, C and an active device (op-amp) in place of inductors; a passive filter uses only R, L and C.

Merits of active filters

  1. No inductors: inductors are large, heavy, lossy (low Q) and pick up magnetic interference, especially at audio frequencies. Active filters avoid them.
  2. Gain: the passband gain can be set above unity, so the filter can also amplify.
  3. Isolation: the op-amp has high input and low output impedance, so stages can be cascaded without interaction; a high-order filter is designed as a cascade of independent biquads.
  4. Tunability: ωo\omega_o, QQ and gain are often adjustable by separate resistors.
  5. Size and cost: small, light and cheap; can be integrated (with switched-capacitor techniques).

Demerits of active filters

  1. Power supply needed: they consume power and need a DC supply.
  2. Limited frequency range: the op-amp's finite gain-bandwidth and slew rate limit use to roughly below 1 MHz; passive LC filters work up to GHz.
  3. Limited signal swing: output saturates near the supply rails, so they cannot handle large voltages or power.
  4. Noise and offset: op-amps add noise, DC offset and distortion.
  5. Higher sensitivity: many active circuits (e.g. Sallen-Key at high Q) are more sensitive to element changes than doubly terminated LC ladders.
  6. Reliability: active devices may fail or drift with temperature.
PointActivePassive
InductorsNot neededNeeded
GainCan exceed 1≤ 1
SupplyNeededNot needed
FrequencyUp to ~MHzUp to GHz
Power handlingLowHigh
CascadingEasyLoading problem
NoiseMoreLess

Typical use: active filters are preferred for low-frequency, low-power applications (audio, instrumentation, biomedical signals), while passive filters are used at RF and where large power must be handled.

Questions from Old Question Collection (BEI EX 606 and BEX EX 704) (Scanned IOE papers: BEI EX 606 2078–2083 and BEX EX 704 2069–2076), Old Question Collection (EX 704) (IOE BEX EX 704 papers from 2069 to 2081) and 2080 course paper (ENEX 301) (IOE ENEX 301 new-course paper, 2082 Chaitra). Answers are written for this site; check them against your class notes.

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