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SECOND ORDER CIRCUITS

Module by: Dinh Sy Hien. E-mail the author

Summary: We will consider circuits containing two storage elements. These are known as second order circuits because their responses are described by differential equations that contain second derivatives.

INTRODUCTION

In previous chapter we considered circuits with a single storage element (a capacitor or an inductor). Such circuits are first-order because the differential equations describing them are first-order. In this chapter we will consider circuits containing two storage elements. These are known as second order circuits because their responses are described by differential equations that contain second derivatives.

Figure 1: Typical examples of second-order circuits: a) series RLC circuit, b) parallel RLC circuit, c) Rl circuit, d) RC circuit.
Figure 1 (graphics1.png)

Typical examples of second-order circuits are RLC circuits, in which the three kinds of passive elements are present. Examples of such circuits are shown in Figure 1(a) and Figure 1(b). Other examples are RC and RL circuits, as shown in Figure 1(c) and Figure 1(d). It is apparent from Figure 1 that a second-order circuit may have two storage elements of different type or the same type (provided elements of the same type cannot be represented by an equivalent single element). An op amp circuit with two storage elements may also be a second-order circuit. As with first-order circuits, a second-order circuit may contain several resistors and dependent and independent sources.

A second-order circuit is characterized by a second-order differential equation. It consists of resistors and the equivalent of two energy storage elements.

Our analysis of second-order circuits will be similar to that used for first-order. We will first consider circuits that are excited by the initial conditions of the storage elements. Although these circuits may contain dependent sources, they are free of independent sources. These source-free circuits will give natural responses as expected. Later we will consider circuits that are excited by independent sources. These circuits will give both the transient response and the steady-state response. We consider only dc independent sources in this chapter.

We begin by learning how to obtain the initial conditions for the circuit variables and their derivatives, as this is crucial to analyzing second-order circuits. Then we consider series and parallel RLC circuits such as shown in Fig 1 for the two cases of excitation: by initial conditions of the energy storage elements and by step inputs. Later we examine other types of second-order circuits.

THE SOURCE-FREE SERIES RLC CIRCUIT

An understanding of the natural response of the series RLC circuit is a necessary background for future studies in filter design and communications networks.

Figure 2: A source-free series RLC circuit.
Figure 2 (graphics2.png)

Consider the series RLC circuit shown in Figure 2. The circuit is being excited by the energy initially stored in the capacitor and inductor. The energy is represented by the initial capacitor voltage V0 and initial inductor current I0. Thus, at t = 0,

v ( 0 ) = 1 C 0 idt = V 0 v ( 0 ) = 1 C 0 idt = V 0 size 12{v \( 0 \) = { {1} over {C} } Int cSub { size 8{ - infinity } } cSup { size 8{0} } { ital "idt"} =V rSub { size 8{0} } } {} (1)
i ( 0 ) = I 0 i ( 0 ) = I 0 size 12{i \( 0 \) =I rSub { size 8{0} } } {} (2)

Applying KVL around the loop in Figure 1,

Ri + L di dt + 1 C t idt = 0 Ri + L di dt + 1 C t idt = 0 size 12{ ital "Ri"+L { { ital "di"} over { ital "dt"} } + { {1} over {C} } Int cSub { size 8{ - infinity } } cSup { size 8{t} } { ital "idt"} =0} {} (3)

To eliminate the integral, we differentiate with respect to t and rearrange terms. We get

d 2 i dt 2 + R L di dt + i LC = 0 d 2 i dt 2 + R L di dt + i LC = 0 size 12{ { {d rSup { size 8{2} } i} over { ital "dt" rSup { size 8{2} } } } + { {R} over {L} } { { ital "di"} over { ital "dt"} } + { {i} over { ital "LC"} } =0} {} (4)

This is a second-order differential equation and is the reason for calling the RLC circuits in this chapter second-order circuits. Our goal is to solve Equation 4. To solve such a second-order differential equation requires that we have two initial conditions, such as the initial value of i and its first derivative or initial values of some i and v. The initial value of i is given in Equation 2. We get the initial value of the derivative of I from Equation 1 and Equation 3; that is,

Ri ( 0 ) + L di ( 0 ) dt + V 0 = 0 Ri ( 0 ) + L di ( 0 ) dt + V 0 = 0 size 12{ ital "Ri" \( 0 \) +L { { ital "di" \( 0 \) } over { ital "dt"} } +V rSub { size 8{0} } =0} {}

Or

di ( 0 ) dt = 1 L ( RI 0 + V 0 ) di ( 0 ) dt = 1 L ( RI 0 + V 0 ) size 12{ { { ital "di" \( 0 \) } over { ital "dt"} } = - { {1} over {L} } \( ital "RI" rSub { size 8{0} } +V rSub { size 8{0} } \) } {} (5)

with the two initial conditions in Equation 2 and Equation 5, we can now solve Equation 4. Our experience in the preceding chapter on first-order circuits suggests that the solution is of exponential form. So we let

i = Ae st i = Ae st size 12{i= ital "Ae" rSup { size 8{ ital "st"} } } {} (6)

where A and s are constants to be determined. Substituting Equation 7 into Equation 5 and carrying out the necessary differentiations, we obtain

As 2 e st + AR L se st + A LC e st = 0 As 2 e st + AR L se st + A LC e st = 0 size 12{ ital "As" rSup { size 8{2} } e rSup { size 8{ ital "st"} } + { { ital "AR"} over {L} } ital "se" rSup { size 8{ ital "st"} } + { {A} over { ital "LC"} } e rSup { size 8{ ital "st"} } =0} {}

Or

Ae st ( s 2 + R L s + 1 LC ) = 0 Ae st ( s 2 + R L s + 1 LC ) = 0 size 12{ ital "Ae" rSup { size 8{ ital "st"} } \( s rSup { size 8{2} } + { {R} over {L} } s+ { {1} over { ital "LC"} } \) =0} {} (7)

Since i=Aesti=Aest size 12{i= ital "Ae" rSup { size 8{ ital "st"} } } {} is assumed solution we are trying to find, only the expression in parentheses can be zero:

s 2 + R L s + 1 LC = 0 s 2 + R L s + 1 LC = 0 size 12{s rSup { size 8{2} } + { {R} over {L} } s+ { {1} over { ital "LC"} } =0} {} (8)

This quadratic equation is known as the characteristic equation of the differential Equation 4, since the roots of the equation dictate the character of i. The two roots of Equation 8 are

s 1 = R 2L + ( R 2L ) 2 1 LC s 1 = R 2L + ( R 2L ) 2 1 LC size 12{s rSub { size 8{1} } = - { {R} over {2L} } + sqrt { \( { {R} over {2L} } \) rSup { size 8{2} } - { {1} over { ital "LC"} } } } {} (9)
s 2 = R 2L ( R 2L ) 2 1 LC s 2 = R 2L ( R 2L ) 2 1 LC size 12{s rSub { size 8{2} } = - { {R} over {2L} } - sqrt { \( { {R} over {2L} } \) rSup { size 8{2} } - { {1} over { ital "LC"} } } } {} (10)

A more compact way of expressing the roots is

s 1 = α + α 2 ω 0 2 , s 2 = α α 2 ω 0 2 s 1 = α + α 2 ω 0 2 , s 2 = α α 2 ω 0 2 size 12{s rSub { size 8{1} } = - α+ sqrt {α rSup { size 8{2} } - ω rSub { size 8{0} } rSup { size 8{2} } } ,s rSub { size 8{2} } = - α - sqrt {α rSup { size 8{2} } - ω rSub { size 8{0} } rSup { size 8{2} } } } {} (11)

Where

α = R 2L , ω 0 = 1 LC α = R 2L , ω 0 = 1 LC size 12{α= { {R} over {2L} } ,ω rSub { size 8{0} } = { {1} over { sqrt { ital "LC"} } } } {} (12)

The roots s1 and s2 are called natural frequencies, measured in nepers per second (Np/s), because they are associated with the natural response of the circuit; ω0 is known as the resonant frequency or strictly as the undamped natural frequency or the damping factor, expressed in nepers per second. In terms of α and ω0, Equation 8 can be written as

s 2 + 2αs + ω 0 2 = 0 s 2 + 2αs + ω 0 2 = 0 size 12{s rSup { size 8{2} } +2αs+ω rSub { size 8{0} } rSup { size 8{2} } =0} {} (13)

The variables s and ω0ω0 size 12{ω rSub { size 8{0} } } {} are important quantities we will be discussing throughout the rest of the text.

The two values of s in Equation 11 indicate that there are two possible solutions for I, each of which is of the form of the assumed solution in Equation 7; that is,

i 1 = A 1 e s 1 t , i 1 = A 1 e s 1 t , size 12{i rSub { size 8{1} } =A rSub { size 8{1} } e rSup { size 8{s rSub { size 6{1} } t} } ,} {} (14)

and

i 2 = A 2 e s 2 t i 2 = A 2 e s 2 t size 12{i rSub { size 8{2} } =A"" lSub { size 8{2} } e rSup { size 8{s rSub { size 6{2} } t} } } {}

Since Equation 4 is a linear equation, any linear combination of the two distinct solutions i1 and i2 is also a solution of Equation 4. A complete or total solution of Equation 4 would therefore require a linear combination of i1i1 size 12{i rSub { size 8{1} } } {} and i2i2 size 12{i rSub { size 8{2} } } {}. Thus, the natural response of the series RLC circuit is

i ( t ) = A 1 e s 1 t + A 2 e s 2 t i ( t ) = A 1 e s 1 t + A 2 e s 2 t size 12{i \( t \) =A rSub { size 8{1} } e rSup { size 8{s rSub { size 6{1} } t} } +A"" lSub {2} size 12{e rSup {s rSub { size 6{2} } t} }} {} (15)

Where the constants A1 and A2 are determined from the initial values i(0) and di(0)/dt in Equation 2 and Equation 5.

From Equation 11, we can infer that there are three types of solutions:

1. If α>ω0α>ω0 size 12{α>ω rSub { size 8{0} } } {}, we have the overdamped case.

2. If α=ω0α=ω0 size 12{α=ω rSub { size 8{0} } } {}, we have the critically damped case.

3. If α<ω0α<ω0 size 12{α<ω rSub { size 8{0} } } {}, we have the underdamped case.

We will consider each of these cases separately.

Overdamped case ( α>ω0α>ω0 size 12{α>ω rSub { size 8{0} } } {})

From Equation 9 and Equation 11, α>ω0α>ω0 size 12{α>ω rSub { size 8{0} } } {} implies C>4L/R2C>4L/R2 size 12{C> {4L} slash {R rSup { size 8{2} } } } {}. When this happens, both roots s1s1 size 12{s rSub { size 8{1} } } {} and s2s2 size 12{s rSub { size 8{2} } } {} are negative and real. The response is

i t = A 1 e s 1 t + A 2 e s 2 t i t = A 1 e s 1 t + A 2 e s 2 t size 12{i left (t right )=A rSub { size 8{1} } e rSup { size 8{s rSub { size 6{1} } t} } +A rSub {2} size 12{e rSup {s rSub { size 6{2} } t} }} {} (16)

which decays and approaches zero as t increases. Figure 3(a) illustrates a typical overdamped response.

Figure 3: a) Overdamped, b) critically damped response, c) underdamped response.
Figure 3 (graphics3.png)

Critically damped case ( α=ω0α=ω0 size 12{α=ω rSub { size 8{0} } } {})

When α=ω0α=ω0 size 12{α=ω rSub { size 8{0} } } {}, C=4L/R2C=4L/R2 size 12{C= {4L} slash {R rSup { size 8{2} } } } {} and

s 1 = s 2 = α = R 2L s 1 = s 2 = α = R 2L size 12{s rSub { size 8{1} } =s rSub { size 8{2} } = - α= - { {R} over {2L} } } {} (17)

For this case, Equation 15 yields

i ( t ) = A 1 e αt + A 2 e αt = A 3 e αt i ( t ) = A 1 e αt + A 2 e αt = A 3 e αt size 12{i \( t \) =A rSub { size 8{1} } e rSup { size 8{ - αt} } +A rSub { size 8{2} } e rSup { size 8{ - αt} } =A rSub { size 8{3} } e rSup { size 8{ - αt} } } {}

Where A3=A1+A2A3=A1+A2 size 12{A rSub { size 8{3} } =A rSub { size 8{1} } +A rSub { size 8{2} } } {}. This cannot be the solution, because the two initial conditions cannot be satisfied with single constant. What then could be wrong? Our assumption of an exponential solution is incorrect for the special case of critical damping. Let us go back to Equation 4. When α=ω0=R/2Lα=ω0=R/2L size 12{α=ω rSub { size 8{0} } = {R} slash {2L} } {}, Equation 4 becomes

d 2 i dt 2 + di dt + α 2 i = 0 d 2 i dt 2 + di dt + α 2 i = 0 size 12{ { {d rSup { size 8{2} } i} over { ital "dt" rSup { size 8{2} } } } +2α { { ital "di"} over { ital "dt"} } +α rSup { size 8{2} } i=0} {}

or

d dt ( di dt + αi ) + α ( di dt + αi ) = 0 d dt ( di dt + αi ) + α ( di dt + αi ) = 0 size 12{ { {d} over { ital "dt"} } \( { { ital "di"} over { ital "dt"} } +αi \) +α \( { { ital "di"} over { ital "dt"} } +αi \) =0} {} (18)

If we let

f = ( di dt + αi ) f = ( di dt + αi ) size 12{f= \( { { ital "di"} over { ital "dt"} } +αi \) } {} (19)

then Equation 18 becomes

df dt + αf = 0 df dt + αf = 0 size 12{ { { ital "df"} over { ital "dt"} } +αf=0} {}

which is a first-order differential equation with solution f=A1eαtf=A1eαt size 12{f=A rSub { size 8{1} } e rSup { size 8{ - αt} } } {}, where A1A1 size 12{A rSub { size 8{1} } } {} is a constant. Equation 19 then becomes

e αt di dt + e αt αi = A 1 e αt di dt + e αt αi = A 1 size 12{e rSup { size 8{αt} } { { ital "di"} over { ital "dt"} } +e rSup { size 8{αt} } αi=A"" lSub { size 8{1} } } {}

or

e αt di dt + e αt αi = A 1 e αt di dt + e αt αi = A 1 size 12{e rSup { size 8{αt} } { { ital "di"} over { ital "dt"} } +e rSup { size 8{αt} } αi=A"" lSub { size 8{1} } } {} (20)

This can be written as

d dt ( e αt i ) = A 1 d dt ( e αt i ) = A 1 size 12{ { {d} over { ital "dt"} } \( e rSup { size 8{αt} } i \) =A rSub { size 8{1} } } {} (21)

Integrating both sides yields

e αt i = A 1 t + A 2 e αt i = A 1 t + A 2 size 12{e rSup { size 8{αt} } i=A rSub { size 8{1} } t+A rSub { size 8{2} } } {}

or

i = ( A 1 t + A 2 ) e αt i = ( A 1 t + A 2 ) e αt size 12{i= \( A rSub { size 8{1} } t+A rSub { size 8{2} } \) e rSup { size 8{ - αt} } } {} (22)

where A2A2 size 12{A rSub { size 8{2} } } {} is another constant. Hence, the natural response of the critically damped circuit is a sum of two terms: a negative exponential and a negative exponential multiplied by a linear term, or

i ( t ) = ( A 2 + A 1 ) e αt i ( t ) = ( A 2 + A 1 ) e αt size 12{i \( t \) = \( A rSub { size 8{2} } +A rSub { size 8{1} } \) e rSup { size 8{ - αt} } } {} (23)

A typical critically damped response is shown in Figure 3(b). In fact, Figure 3(b) is a sketch of i(t)=teαti(t)=teαt size 12{i \( t \) = ital "te" rSup { size 8{ - αt} } } {}, which reaches a maximum value of e1/αe1/α size 12{ {e rSup { size 8{ - 1} } } slash {α} } {} at t=1/αt=1/α size 12{t= {1} slash {α} } {}, one time constant, and the decays all the way to zero.

Underdamped case ( α<ω0α<ω0 size 12{α<ω rSub { size 8{0} } } {})

For α<ω0α<ω0 size 12{α<ω rSub { size 8{0} } } {}, C<4L/R2C<4L/R2 size 12{C< {4L} slash {R rSup { size 8{2} } } } {}. The roots may be written as

s 1 = α + ( ω 0 2 α 2 ) = α + d s 1 = α + ( ω 0 2 α 2 ) = α + d size 12{s rSub { size 8{1} } = - α+ sqrt { - \( ω rSub { size 8{0} } rSup { size 8{2} } - α rSup { size 8{2} } \) } = - α+jω rSub { size 8{d} } } {} (24)
s 2 = α ( ω 0 2 α 2 ) = α d s 2 = α ( ω 0 2 α 2 ) = α d size 12{s rSub { size 8{2} } = - α - sqrt { - \( ω rSub { size 8{0} } rSup { size 8{2} } - α rSup { size 8{2} } \) } = - α - jω rSub { size 8{d} } } {} (25)

Where j=1j=1 size 12{j= sqrt { - 1} } {}and ωd=ω02α2ωd=ω02α2 size 12{ω rSub { size 8{d} } = sqrt {ω rSub { size 8{0} } rSup { size 8{2} } - α rSup { size 8{2} } } } {}, which is called the damping frequency. Both ω0ω0 size 12{ω rSub { size 8{0} } } {} and ωdωd size 12{ω rSub { size 8{d} } } {} are natural frequencies because they help determine the natural response; while

ω0ω0 size 12{ω rSub { size 8{0} } } {} is often called the undamped natural frequency, ωdωd size 12{ω rSub { size 8{d} } } {} is called the damped natural frequency. The natural response is

i ( t ) = A 1 e ( α d ) t + A 2 e ( α + d ) t = e αt ( A 1 e d t + A 2 e d t ) i ( t ) = A 1 e ( α d ) t + A 2 e ( α + d ) t = e αt ( A 1 e d t + A 2 e d t ) alignl { stack { size 12{i \( t \) =A rSub { size 8{1} } e rSup { size 8{ - \( α - jω rSub { size 6{d} } \) t} } +A rSub {2} size 12{e rSup { - \( α+jω rSub { size 6{d} } \) t} }} {} # size 12{ {}=e rSup { size 8{ - αt} } \( A rSub { size 8{1} } e rSup { size 8{jω rSub { size 6{d} } t} } +A rSub {2} size 12{e rSup { - jω rSub { size 6{d} } t} } size 12{ \) }} {} } } {} (26)

Using Euler’s identities,

e = cos θ + j sin θ , e = cos θ j sin θ e = cos θ + j sin θ , e = cos θ j sin θ size 12{e rSup { size 8{jθ} } ="cos"θ+j"sin"θ,e rSup { size 8{ - jθ} } ="cos"θ - j"sin"θ} {} (27)

We get

i ( t ) = e αt [ A 1 ( cos ω d t + j sin ω d t ) + A 2 ( cos ω d t j sin ω d t ) e αt [ ( A 1 + A 2 ) cos ω d t + j ( A 1 A 2 ) sin ω d t ] i ( t ) = e αt [ A 1 ( cos ω d t + j sin ω d t ) + A 2 ( cos ω d t j sin ω d t ) e αt [ ( A 1 + A 2 ) cos ω d t + j ( A 1 A 2 ) sin ω d t ] alignl { stack { size 12{i \( t \) =e rSup { size 8{ - αt} } \[ A rSub { size 8{1} } \( "cos"ω rSub { size 8{d} } t+j"sin"ω rSub { size 8{d} } t \) +A rSub { size 8{2} } \( "cos"ω rSub { size 8{d} } t - j"sin"ω rSub { size 8{d} } t \) } {} # =e rSup { size 8{ - αt} } \[ \( A rSub { size 8{1} } +A rSub { size 8{2} } \) "cos"ω rSub { size 8{d} } t+j \( A rSub { size 8{1} } - A rSub { size 8{2} } \) "sin"ω rSub { size 8{d} } t \] {} } } {} (28)

Replacing constants (A1+A2)(A1+A2) size 12{ \( A rSub { size 8{1} } +A rSub { size 8{2} } \) } {} and j(A1A2)j(A1A2) size 12{j \( A rSub { size 8{1} } - A rSub { size 8{2} } \) } {} with constants B1B1 size 12{B rSub { size 8{1} } } {} and B2B2 size 12{B rSub { size 8{2} } } {}, we write

i ( t ) = e αt [ ( B 1 cos ω d t + j ( B 2 ) sin ω d t ] i ( t ) = e αt [ ( B 1 cos ω d t + j ( B 2 ) sin ω d t ] size 12{i \( t \) =e rSup { size 8{ - αt} } \[ \( B rSub { size 8{1} } "cos"ω rSub { size 8{d} } t+j \( B rSub { size 8{2} } \) "sin"ω rSub { size 8{d} } t \] } {} (29)

With the presence of sine and cosine functions, it is clear that the natural response for this case is exponentially damped and oscillatory in nature. The response has a time constant of 1/α1/α size 12{ {1} slash {α} } {} and a period of T=/ωdT=/ωd size 12{T= {2π} slash {ω rSub { size 8{d} } } } {}. Figure 3(c) depicts a typical underdamped response. Figure 3 assumes for each case that i(0) = 0.

Once the inductor current i(t) is found for RLC series circuits as shown above, other circuit quantities such as individual element voltages can easily be found. For example, the resistor voltage is vR=RivR=Ri size 12{v rSub { size 8{R} } = ital "Ri"} {}, and the inductor voltage is vL=Ldi/dtvL=Ldi/dt size 12{v rSub { size 8{L} } =L { ital "di"} slash { ital "dt"} } {}. The inductor current i(t) is selected as the key variable to be determined first in order to take advantage of Equation 2.

We conclude this section by noting the following interesting, peculiar properties of an RLC network:

1. The behavior of such a network is captured by the idea of damping, which is the gradual loss of the initial stored energy, as evidenced by the continuous decrease in the amplitude of the response. The damping effect is due to the presence of the resistance R. The damping factor  determines the rate at which the response is damped. If R = 0, then α=0α=0 size 12{α=0} {}, and we have an LC circuit with 1/LC1/LC size 12{ {1} slash { sqrt { ital "LC"} } } {}as the undamped natural frequency. Since α<ω0α<ω0 size 12{α<ω rSub { size 8{0} } } {} in this case, the response is not only undamped but also oscillatory. The circuit is said to be lossless, because dissipating or damping element (R) is absent. By adjusting the value of R, the response may be made undamped, overdamped, critically damped, or underdamped.

2. Oscillatory response is possible due to the presence of the two types of storage elements. Having both L and C allows the flow of energy back and forth between the two. The damped oscillation exhibited by the underdamped response is known as ringing. It stems from the ability of the storage elements L and C to transfer energy back and forth between them.

3. Observe from Figure 3 that the waveforms of the responses differ. In general, it is difficult to tell from the waveforms the difference between the overdamped and critically damped responses. The critically damped case is the borderline between the underdamped and overdamped cases and it decays the fastest. With the same initial conditions, the overdamped case has the longest settling time, because it takes the longest time to dissipate the initial stored energy. If we desire the the fastest response without oscillation or ringing, the critically damped circuit is right choice.

THE SOURCE-FREE PARALLEL RLC CIRCUIT

Parallel RLC circuits find many practical applications, notably in communications networks and filter designs.

Consider the parallel RLC circuit shown in Figure 4. Assume initial inductor current I0 and initial capacitor voltage V0,

i ( 0 ) = I 0 = 1 L 0 v ( t ) dt i ( 0 ) = I 0 = 1 L 0 v ( t ) dt size 12{i \( 0 \) =I rSub { size 8{0} } = { {1} over {L} } Int cSub { size 8{ infinity } } cSup { size 8{0} } {v \( t \) ital "dt"} } {} (30)
v ( 0 ) = V 0 v ( 0 ) = V 0 size 12{v \( 0 \) =V rSub { size 8{0} } } {} (31)

Since the three elements are in parallel, they have the same voltage v across them. According to passive sign convention, the current is entering each element; that is, the current through each element is leaving the top node. Thus, applying KCL at the top node gives

v R + 1 L t vdt + C dv dt = 0 v R + 1 L t vdt + C dv dt = 0 size 12{ { {v} over {R} } + { {1} over {L} } Int cSub { size 8{ - infinity } } cSup { size 8{t} } { ital "vdt"} +C { { ital "dv"} over { ital "dt"} } =0} {} (32)
Figure 4: A source-free parallel RLC.
Figure 4 (graphics4.png)

Taking the derivative with respect to t and dividing by C results in

d 2 v dt 2 + 1 RC dv dt + 1 LC v = 0 d 2 v dt 2 + 1 RC dv dt + 1 LC v = 0 size 12{ { {d rSup { size 8{2} } v} over { ital "dt" rSup { size 8{2} } } } + { {1} over { ital "RC"} } { { ital "dv"} over { ital "dt"} } + { {1} over { ital "LC"} } v=0} {} (33)

We obtain the characteristic equation by replacing the first derivative by s and the second derivative by s 2 s 2 size 12{s rSup { size 8{2} } + { {1} over { ital "RC"} } s+ { {1} over { ital "LC"} } =0} {} . By following the same reasoning used in establishing Equation 4 through Equation 8, the characteristic equation is obtained as

s 2 + 1 RC s + 1 LC = 0 s 2 + 1 RC s + 1 LC = 0 size 12{s rSup { size 8{2} } + { {1} over { ital "RC"} } s+ { {1} over { ital "LC"} } =0} {} (34)

The roots of the characteristic equations are

s 1,2 = 1 2 RC ± ( 1 2 RC ) 2 1 LC s 1,2 = 1 2 RC ± ( 1 2 RC ) 2 1 LC size 12{s rSub { size 8{1,2} } = - { {1} over {2 ital "RC"} } +- sqrt { \( { {1} over {2 ital "RC"} } \) rSup { size 8{2} } - { {1} over { ital "LC"} } } } {}

Or

s 1,2 = α ± α 2 ω 0 2 s 1,2 = α ± α 2 ω 0 2 size 12{s rSub { size 8{1,2} } = - α +- sqrt {α rSup { size 8{2} } - ω rSub { size 8{0} } rSup { size 8{2} } } } {} (35)

Where

α = 1 2 RC , ω 0 = 1 LC α = 1 2 RC , ω 0 = 1 LC size 12{α= { {1} over {2 ital "RC"} } ,ω rSub { size 8{0} } = { {1} over { sqrt { ital "LC"} } } } {} (36)

The names of these terms remain the same as in the preceding section, as they play the same role in the solution. Again, there are three possible solutions, depending on whether α>ω0α>ω0 size 12{α>ω rSub { size 8{0} } } {}, α=ω0α=ω0 size 12{α=ω rSub { size 8{0} } } {}, or α<ω0α<ω0 size 12{α<ω rSub { size 8{0} } } {}. Let us consider these cases separately.

Overdamped case ( α>ω0α>ω0 size 12{α>ω rSub { size 8{0} } } {})

From Equation 36, α>ω0α>ω0 size 12{α>ω rSub { size 8{0} } } {} when L>4R2CL>4R2C size 12{L>4R rSup { size 8{2} } C} {}. The roots of characteristic equation are real and negative. The response is

v ( t ) = A 1 e s 1 t + A 2 e s 2 t v ( t ) = A 1 e s 1 t + A 2 e s 2 t size 12{v \( t \) =A rSub { size 8{1} } e rSup { size 8{s"" lSub { size 6{1} } t} } +A rSub {2} size 12{e rSup {s rSub { size 6{2} } t} }} {} (37)

Critically damped case ( α=ω0α=ω0 size 12{α=ω rSub { size 8{0} } } {})

For α=ω0α=ω0 size 12{α=ω rSub { size 8{0} } } {}, L=4R2CL=4R2C size 12{L=4R rSup { size 8{2} } C} {}. The roots are real and equal so that the response is

v ( t ) = ( A 1 + A 2 t ) e αt v ( t ) = ( A 1 + A 2 t ) e αt size 12{v \( t \) = \( A rSub { size 8{1} } +A rSub { size 8{2} } t \) e rSup { size 8{ - αt} } } {} (38)

Underdamped case ( α<ω0α<ω0 size 12{α<ω rSub { size 8{0} } } {})

When α<ω0α<ω0 size 12{α<ω rSub { size 8{0} } } {}, L<4R2CL<4R2C size 12{L<4R rSup { size 8{2} } C} {}. In this case the roots are complex and may be expressed as

s 1,2 = α ± d s 1,2 = α ± d size 12{s rSub { size 8{1,2} } = - α +- sqrt {α rSup { size 8{2} } - ω rSub { size 8{0} } rSup { size 8{2} } } } {} (39)

Where

ω d = ω 0 2 α 2 ω d = ω 0 2 α 2 size 12{ω"" lSub { size 8{d} } = sqrt {ω rSub { size 8{0} } rSup { size 8{2} } - α rSup { size 8{2} } } } {} (40)

The response is

v ( t ) = e αt ( A 1 cos ω d t + A 2 sin ω d t ) v ( t ) = e αt ( A 1 cos ω d t + A 2 sin ω d t ) size 12{v \( t \) =e rSup { size 8{ - αt} } \( A rSub { size 8{1} } "cos"ω rSub { size 8{d} } t+A rSub { size 8{2} } "sin"ω rSub { size 8{d} } t \) } {} (41)

The constants A1 and A2 in each case can be determined from the initial conditions. We need v(0) and dv(0)/dt. The first term is known from Equation 31. We find the second term by combining Equation 30 and Equation 32, as

V 0 R + I 0 + C dv ( 0 ) dt = 0 V 0 R + I 0 + C dv ( 0 ) dt = 0 size 12{ { {V rSub { size 8{0} } } over {R} } +I rSub { size 8{0} } +C { { ital "dv" \( 0 \) } over { ital "dt"} } =0} {}

Or

dv ( 0 ) dt = ( V 0 + RI 0 ) RC dv ( 0 ) dt = ( V 0 + RI 0 ) RC size 12{ { { ital "dv" \( 0 \) } over { ital "dt"} } = - { { \( V rSub { size 8{0} } + ital "RI" rSub { size 8{0} } \) } over { ital "RC"} } } {} (42)

The voltage waveforms are similar to those shown in Figure 3 and will depend on whether the circuit is overdamped, underdamped, or critically damped.

Having found the capacitor voltage v(t) for the parallel RLC circuit as shown above, we can readily obtain other circuit quantities such as individual circuits. For example, the resistor current is iR=v/RiR=v/R size 12{i rSub { size 8{R} } = {v} slash {R} } {} nd the capacitor current is iC=Cdv/dtiC=Cdv/dt size 12{i rSub { size 8{C} } =C { ital "dv"} slash { ital "dt"} } {}. We have selected the capacitor voltage is v(t) as the key variable to be determined first in order to take i(t) for the RLC series circuit, whereas we first found the capacitor voltage v(t) for the parallel RLC circuit.

STEP RESPONSE OF A SERIES RLC CIRCUIT

As we learned in the preceding chapter, the step response is obtained be the sudden application of a dc source. Consider the series RLC circuit shown in Figure 5. Applying KVL around the loop for tt size 12{t} {}.

L di dt + Ri + v = V s L di dt + Ri + v = V s size 12{L { { ital "di"} over { ital "dt"} } + ital "Ri"+v=V rSub { size 8{s} } } {} (43)

But

i = C dv dt i = C dv dt size 12{i=C { { ital "dv"} over { ital "dt"} } } {}

Substituting for I in Equation 43 and rearranging terms,

d 2 v dt 2 + R L dv dt + v LC = V s LC d 2 v dt 2 + R L dv dt + v LC = V s LC size 12{ { {d rSup { size 8{2} } v} over { ital "dt" rSup { size 8{2} } } } + { {R} over {L} } { { ital "dv"} over { ital "dt"} } + { {v} over { ital "LC"} } = { {V rSub { size 8{s} } } over { ital "LC"} } } {} (44)

which has the same form as Equation 4. More specially, the coefficients are the same (and that is important in determining the frequency parameters) but the variable is different. Hence, the characteristic equation for the series RLC circuit is not affected by the presence of the dc source.

The solution to the Equation 44 has two components: the transient response vt(t)vt(t) size 12{v rSub { size 8{t} } \( t \) } {} and the steady-state response vss(t)vss(t) size 12{v rSub { size 8{ ital "ss"} } \( t \) } {}; that is,

v ( t ) = v t ( t ) + v ss ( t ) v ( t ) = v t ( t ) + v ss ( t ) size 12{v \( t \) =v rSub { size 8{t} } \( t \) +v rSub { size 8{ ital "ss"} } \( t \) } {} (45)

The transient response vt(t)vt(t) size 12{v rSub { size 8{t} } \( t \) } {} is the component of the total response that dies out with time. The form of the transient response is the same as the form of the solution obtained in section 2 for the source-free circuit, given by Equation 16, Equation 23 and Equation 29. Therefore, the transient response vt(t)vt(t) size 12{v rSub { size 8{t} } \( t \) } {} for the overdamped, underdamped, and critically damped cases are:

vt(t)=A1es1t+A2es2tvt(t)=A1es1t+A2es2t size 12{v rSub { size 8{t} } \( t \) =A rSub { size 8{1} } e rSup { size 8{s rSub { size 6{1} } t} } +A rSub {2} size 12{e rSup {s rSub { size 6{2} } t} }} {}(46)

`Overdamped

vt(t)=(A1+A2t)eαtvt(t)=(A1+A2t)eαt size 12{v rSub { size 8{t} } \( t \) = \( A rSub { size 8{1} } +A"" lSub { size 8{2} } t \) e rSup { size 8{ - αt} } } {}(47)

Critcally damped

vt(t)=(A1cosωdt+A2sinωdt)eαtvt(t)=(A1cosωdt+A2sinωdt)eαt size 12{v rSub { size 8{t} } \( t \) = \( A rSub { size 8{1} } "cos"ω rSub { size 8{d} } t+A"" lSub { size 8{2} } "sin"ω rSub { size 8{d} } t \) e rSup { size 8{ - αt} } } {} (48)

Underdamped

Figure 5: Step voltage applied to a series RLC circuit.
Figure 5 (graphics5.png)

The steady-state response is the final value of v(t). In the circuit in Figure 5, the final value of the capacitor voltage is the same as the source voltage Vs. Hence,

v ss ( t ) = v ( ) = V s v ss ( t ) = v ( ) = V s size 12{v rSub { size 8{ ital "ss"} } \( t \) =v \( infinity \) =V rSub { size 8{s} } } {} (49)

Thus, the complete solutions for the overdamped, and critically dadmped cases are:

vt(t)=Vs+A1es1t+A2es2tvt(t)=Vs+A1es1t+A2es2t size 12{v rSub { size 8{t} } \( t \) =V rSub { size 8{s} } +A rSub { size 8{1} } e rSup { size 8{s rSub { size 6{1} } t} } +A rSub {2} size 12{e rSup {s rSub { size 6{2} } t} }} {}(50)

Overdamped

vt(t)=Vs+(A1+A2t)eαtvt(t)=Vs+(A1+A2t)eαt size 12{v rSub { size 8{t} } \( t \) =V rSub { size 8{s} } + \( A rSub { size 8{1} } +A"" lSub { size 8{2} } t \) e rSup { size 8{ - αt} } } {}(51)

Critically damped

vt(t)=Vs+(A1cosωdt+A2sinωdt)eαtvt(t)=Vs+(A1cosωdt+A2sinωdt)eαt size 12{v rSub { size 8{t} } \( t \) =V rSub { size 8{s} } + \( A rSub { size 8{1} } "cos"ω rSub { size 8{d} } t+A"" lSub { size 8{2} } "sin"ω rSub { size 8{d} } t \) e rSup { size 8{ - αt} } } {}(52)

Underdamped

The values of constants A1A1 size 12{A rSub { size 8{1} } } {} and A2A2 size 12{A rSub { size 8{2} } } {} are obtained from the initial conditions: v(0) and dv(0)/dt. Keep in mind that v and i are, respectively, the voltage across the capacitor and the current through the inductor. Therefore, Equation 50 only applies for the finding v. But once the capacitor voltage vC=vvC=v size 12{v rSub { size 8{C} } =v} {} s known, we can determine I=Cdv/dtI=Cdv/dt size 12{I=C { ital "dv"} slash { ital "dt"} } {}, which is the same current through the capacitor, inductor, and resistor. Hence, the voltage across the resistor is vR=iRvR=iR size 12{v rSub { size 8{R} } = ital "iR"} {}, while the inductor voltage is vL=Ldi/dtvL=Ldi/dt size 12{v rSub { size 8{L} } =L { ital "di"} slash { ital "dt"} } {}.

Alternatively, the complete response for any variable x(t) can be found directly, because it has the general form

x ( t ) = x ss ( t ) + x t ( t ) x ( t ) = x ss ( t ) + x t ( t ) size 12{x \( t \) =x rSub { size 8{ ital "ss"} } \( t \) +x rSub { size 8{t} } \( t \) } {} (53)

Where the xss=x()xss=x() size 12{x rSub { size 8{ ital "ss"} } =x \( infinity \) } {} is the final value and xt(t)xt(t) size 12{x rSub { size 8{t} } \( t \) } {} is the transient response. The final value is found as in Section 1. The transient response has the same form as in Equation 46, and the associated constants are determined from Equation 50 based on the values of x(0) and dx(0)/dtdx(0)/dt size 12{ { ital "dx" \( 0 \) } slash { ital "dt"} } {}.

STEP RESPONSE OF A PARALLEL RLC CIRCUIT

Consider the parallel RLC circuit shown in Figure 6. We want to find i due to a sudden application of a dc current. Applying KCL at the top node for t > 0,

v R + i + C dv dt = I s v R + i + C dv dt = I s size 12{ { {v} over {R} } +i+C { { ital "dv"} over { ital "dt"} } =I rSub { size 8{s} } } {} (54)

But

v = L di dt v = L di dt size 12{v=L { { ital "di"} over { ital "dt"} } } {}

Substituting for v in Equation 54 and dividing by LC, we get

d 2 i dt 2 + 1 RC di dt + i LC = I s LC d 2 i dt 2 + 1 RC di dt + i LC = I s LC size 12{ { {d rSup { size 8{2} } i} over { ital "dt" rSup { size 8{2} } } } + { {1} over { ital "RC"} } { { ital "di"} over { ital "dt"} } + { {i} over { ital "LC"} } = { {I rSub { size 8{s} } } over { ital "LC"} } } {} (55)

Which has the same characteristic equation as Equation 33.

Figure 6: Parallel RLC circuit with an applied current.
Figure 6 (graphics6.png)

The complete solution to Equation 56 consists of the transient response it(t)it(t) size 12{i rSub { size 8{t} } \( t \) } {} and the steady-state response ississ size 12{i rSub { size 8{ ital "ss"} } } {}; that is,

i ( t ) = i t ( t ) + i ss ( t ) i ( t ) = i t ( t ) + i ss ( t ) size 12{i \( t \) =i rSub { size 8{t} } \( t \) +i rSub { size 8{ ital "ss"} } \( t \) } {} (56)

The transient response is the same as what we had in section 2. The steady-state response is the final value of i. in the circuit in Figure 6, the final value of the current through the inductor is the same as the source current IsIs size 12{I rSub { size 8{s} } } {}. Thus,

i(t)=Is+A1es1t+A2es2ti(t)=Is+A1es1t+A2es2t size 12{i \( t \) =I rSub { size 8{s} } +A rSub { size 8{1} } e rSup { size 8{s rSub { size 6{1} } t} } +A rSub {2} size 12{e rSup {s rSub { size 6{2} } t} }} {}(Overdamped)

i(t)=Is+(A1+A2t)eαti(t)=Is+(A1+A2t)eαt size 12{i \( t \) =I rSub { size 8{s} } + \( A rSub { size 8{1} } +A rSub { size 8{2} } t \) e rSup { size 8{ - αt} } } {}(57)

(Critically…damped)

i(t)=Is+(A1cosωdt+A2sinωdt)eαti(t)=Is+(A1cosωdt+A2sinωdt)eαt size 12{i \( t \) =I rSub { size 8{s} } + \( A rSub { size 8{1} } "cos"ω rSub { size 8{d} } t+A rSub { size 8{2} } "sin"ω rSub { size 8{d} } t \) e rSup { size 8{ - αt} } } {}(Underdamped)

The constants A1A1 size 12{A rSub { size 8{1} } } {} and A2A2 size 12{A rSub { size 8{2} } } {} in each case can be determined from the initial conditions for i and di/dt. Again, we should keep in mind that Equation 57 only applies for finding the inductor current i. but once the inductor current iL=iiL=i size 12{i rSub { size 8{L} } =i} {} is known, we can find v = L di/dt, which is the same voltage across inductor, capacitor and resistor. Hence, the current through the resistor is iR=v/RiR=v/R size 12{i rSub { size 8{R} } = {v} slash {R} } {} while the capacitor current is iC=dv/dtiC=dv/dt size 12{i rSub { size 8{C} } = { ital "dv"} slash { ital "dt"} } {}. Alternatively, the complete response for any variable x(t) may be found directly using

v ( t ) = x ss ( t ) + x t ( t ) v ( t ) = x ss ( t ) + x t ( t ) size 12{v \( t \) =x rSub { size 8{ ital "ss"} } \( t \) +x rSub { size 8{t} } \( t \) } {} (58)

where xssxss size 12{x rSub { size 8{ ital "ss"} } } {} and xtxt size 12{x rSub { size 8{t} } } {} are its final value and transient response, respectively.

GENERAL SECOND-ORDER CIRCUITS

Now that we have mastered series and parallel RLC circuits, we are prepared to apply the ideas to any second-order circuit having one or more independent sources with constant values. Although the series and parallel RLC circuits are the second-order circuits of greatest interest, second-order circuits including op amp are also useful. Given a second-order circuit, we determine its step response x(t) which may be voltage or current by taking the following four steps:

  1. We first determine the initial conditions v(0) and dx(0)/dt and the final value x()x() size 12{x \( infinity \) } {} as discussed in section 1.
  2. We find the transient response xt(t)xt(t) size 12{x rSub { size 8{t} } \( t \) } {} by applying KCL and KVL. Once a second-order differential equation is obtained, the response is overdamped, critically damped, or underdamped, we obtain xt(t)xt(t) size 12{x rSub { size 8{t} } \( t \) } {} with two unknown constants as we did in previous sections.
  3. We obtain the forced response as
x f ( t ) = x ( ) x f ( t ) = x ( ) size 12{x rSub { size 8{f} } \( t \) =x \( infinity \) } {} (59)

where x()x() size 12{x \( infinity \) } {} is the final value of x, obtained in step 1.

  1. The total response is now found as the sum of the transient response and steady-state response
x ( t ) = x t ( t ) + x ss ( t ) x ( t ) = x t ( t ) + x ss ( t ) size 12{x \( t \) =x rSub { size 8{t} } \( t \) +x rSub { size 8{ ital "ss"} } \( t \) } {} (60)

We finally determine the constants associated with the transient response by imposing the initial conditions x(0) and dx(0)/dt, determined in step 1.

We can apply this general procedure to find the step response of any second-order circuit, including those with op amps.

DUALITY

The concept of duality is a time-saving circuit, effort-effective measure of solving circuit problems. Consider the similarity between Equation 4 and Equation 33. The two equation are the same, except that we must interchange the following quantities: (1) voltage and current, resistance and conductance, (2 capacitance and inductance. Thus, it sometimes occurs in circuit analysis that two different circuits have the same equations and solutions, except that the roles of certain complementary elements are interchanged. This interchangeability is known as the principle of duality.

The duality principle asserts a parallelism between pairs of characterizing equations and theorems of electric circuits.

Dual pairs are shown in Table 1. Note that power does not appear in Table 1, because power has no dual. The reason for this is the principle of linearity; since power is not linear, duality does not apply. Also notice from Table 1 that the principle of duality extends to circuit elements, configurations, and theorems.

Two circuits that are described by equations of the same form, but in which the variables are interchanged, are said to be dual to each other.

Two circuits are said to be dual of one another if they are described by the same characterizing equations with dual quantities interchanged.

Dual pairs.

Table 1
Resistance R Conductance G
Inductance L Capacitance C
Voltage v Current i
Voltage source Current source
Node Mesh
Series path Parallel path
Open circuit Short circuit
KVL KCL
Thevenin Norton

The usefulness of the duality principle is self-evident. Once we know the solution to one circuit, we automatically have the solution for the dual circuit. It is obvious that the circuits in Figure 4 and Figure 6 are dual. Consequently, the result in Equation 36 is the dual of that in Equation 12. We must keep in mind that the principle of duality is limited to planar circuits. Nonplanar circuits have no duals, as they cannot be described by a system of mesh equations.

To find the dual of a given circuit, we do not need to write down the mesh or node equations. We can a graphic technique. Given a planar circuit, we construct the dual circuit by taking the following three steps:

  1. Place a node at the center of each mesh of given circuit. Place the reference node (the ground) of dual circuit outside the given circuit.
  2. Draw lines between the nodes such that each line crosses an element. Replace that element by its dual (see Table 1).
  3. To determine the polarity of voltage source and direction of current sources, follow this rule. A voltage source that produces a positive (clockwise) mesh current has as its dual a current source whose reference direction is from the ground to the nonreference node.

In case of doubt, one may verify the dual circuit by writing the nodal or mesh equations. The mesh (or nodal) equations of the original circuit are similar to the nodal (or mesh) equations of the dual circuit.

SUMMARY

  1. The RLC circuit is second order because it is described by a second-order differential equations. Its characteristic equation is s2+2αs+ω02=0s2+2αs+ω02=0 size 12{s rSup { size 8{2} } +2αs+ω rSub { size 8{0} } rSup { size 8{2} } =0} {}, where αα size 12{α} {} is damping factor and 0 is the undamped natural frequency. For a series circuit, α=R/2Lα=R/2L size 12{α= {R} slash {2L} } {}, for a parallel circuit α=1/2RCα=1/2RC size 12{α= {1} slash {2 ital "RC"} } {}, and for both cases ω0=1LCω0=1LC size 12{ω rSub { size 8{0} } = { {1} over { sqrt { ital "LC"} } } } {}.
  2. If there are no independent sources in the circuit after switching (or sudden change), we regard the circuit as source-free. The complete solution is natural response.
  3. The natural response of an RLC circuit is over-damped, under-damped, or critically damped, depending on the roots of the characteristic equation. The response is critically damped when the roots are real and equal ( s1=s2s1=s2 size 12{s rSub { size 8{1} } =s rSub { size 8{2} } } {} or α=ω0α=ω0 size 12{α=ω rSub { size 8{0} } } {}), over-damped when the roots are real and unequal ( s1s2s1s2 size 12{s rSub { size 8{1} } <> s rSub { size 8{2} } } {} or α>ω0α>ω0 size 12{α>ω rSub { size 8{0} } } {} ), or under-damped when the roots are complex conjugate ( s1=s2s1=s2 size 12{s rSub { size 8{1} } =s rSub { size 8{2} } } {} or α<ω0α<ω0 size 12{α<ω rSub { size 8{0} } } {}).
  4. If independent sources are present in the circuit after switching, the complete response is the sum of the transient response and the steady-state response.

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