Chapter #7 -- First and Second Order Circuits

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Circuit Theory

Chapter 7 : First and Second Order Circuits

• Here, order refers to the number of capacitors and inductors

• First Order Circuits : The circuits which contain only one capacitor or only one inductor.

• First Order RC Circuits : Such circuits contain independent and dependent sources, resistors + one capacitor.

R

T i

C i

+ v

− v

T

+ v

C

C

• KVL : v

T

= R

T i

C

+ v

C i

C

= C dv

C dt

⇒ v

T

= R

T

C dv

C dt

+ v

C dv

C dt

+

1

R

T

C v

C

=

1

R

T

C

V

T

• Result is a first order ODE

+ v i v s

C

• v

C

= v s

, i

C

= C dv s dt i s

+ i v

C i

C

= i s

, v

C

= v

C

( t

0

)+

1

C

R t t

0 i s

( τ ) dτ

1

• First Order RL Circuits : Such circuits contain independent and dependent sources, resistors + one inductor.

i

+ v

− i

N

+

R

N

− v

L i

L

L

• KCL : i

N

= G

N v

L

+ i

L v

L

= L di

L dt

⇒ i

N

= G

N

L di

L dt

+ i

L di

L dt

+

1

G

N

L i

L

=

1

G

N

L i

N

G

N

=

R

1

N

• Result is a first order ODE v s

+ v i

L i s

+ i v

L

• v

L

= v s

, i

L

= i

L

( t

0

)+

1

L

R t t

0 v s

( τ ) dτ i

L

= i s

, v

L

= L di s dt

2

• Step Response of First Order RC / RL Circuits :

• Here we have DC sources, i.e.

V

T and i

N are constants

• dv

C dt

+

1

R

T

C v

C

=

1

R

T

C

V

T di dt

L +

1

G

N

L i

L

=

1

G

N

L i

N

• These two equations can be combined into a single equation :

• dx dt

+

1

τ x =

1

τ x

• For RC circuits, x = v

C

, τ = R

T

C , x

= V

T

• For RL circuits, x = i

L

, τ = G

N

L =

R

L

N

, x

= i

N

• τ : Time Constant.

• Unit : [ τ ] = Ω sec

(for RC case) =

Ω sec

(for RL case) = sec

• Solution of the ODE : Since x

∞ is constant, dx

∞ dt

= 0

• d ( x − x

) dt

+

1

τ

( x − x

) = 0

• Define a new variable y ( t ) = x ( t ) − x

⇒ dy dt

+

1

τ y = 0

• Solution is : y ( t ) = y ( t

0

) e − t − t

0

τ

• x ( t ) − x

= ( x ( t

0

) − x

) e − t − t

0

τ

For RC Case :

For RL Case : v

C

( t ) − V

T

= ( v

C

( t

0

) − V

T

) e

− t − t

0

RT C i

L

( t ) − i

N

= ( i

L

( t

0

) − i

N

) e

− t − t

0

GN L

3

• Why x

? assume that τ > 0 and take limit as t → ∞

• lim t →∞ x ( t ) = x

+ lim t →∞

( x ( t

0

) − x

) e − t − t

0

τ

= x

3

2.5

4

3.5

5

4.5

2

1.5

1

0 1 2 3 4 5 t (sec)

6 7 8 9 10

• Question : Practically, how long should we wait till we safely assume that x ( t ) ≈ x

. This is called the steady state

• Practically, we have x ( t ) ≈ x

, for t − t

0

> 5 τ

• x ( t ) − x

≈ ( x ( t

0

) − x

) e − 5 ≈ 0 .

006( x ( t

0

) − x

)

• In the above figure, we have τ = 1 sec .

4

• For RC Case : lim t →∞ v

C

( t ) = V

T

⇒ lim t →∞ i

C

( t ) = 0

• In the steady state, capacitor behaves like an open circuit .

• For RL Case : lim t →∞ i

L

( t ) = i

N

⇒ lim t →∞ v

L

( t ) = 0

• In the steady state, inductor behaves like a short circuit .

• Example 1 : Example 7.8. p. 300.

• Since the switch is open for a long time, we may assume that inductor reaches its steady state → short circuit !

• By shorting the inductor → i

L

(0) =

R

1

V

A

+ R

2

• This shows a way to set up the initial condition for inductors.

• For t > 0, the switch is closed. If we wait long enough, we may assume that inductor reaches its steady state → short circuit !

• i

L

( ∞ ) = x

= i

N

=

V

A

R

1

• For t > 0, the switch is closed → τ = G

1

L =

L

R

1

• i

L

( t ) =

V

A

R

1

+(

R

1

V

A

+ R

2

V

A

R

1

) e

− t − t

0

G

1

L

=

V

A

R

1

+(

R

1

V

A

+ R

2

V

R

A

1

) e −

R

1( t − t

0)

L

• v

L

( t ) = L di

L

( t ) dt

= −

1

G

1

(

R

1

V

A

+ R

2

V

A

R

1

) e

− t − t

0

G

1

L

→ 0

5

• Example 2 : Example 7.9. p. 301.

• Since the switch is closed for a long time, we may assume that capacitor reaches its steady state → open circuit !

• By opening the capacitor → v

C

(0) =

V

R

1

A

R

+ R

1

2

• For t > 0, the switch is opened. If we wait long enough, we may assume that capacitor reaches its steady state → open circuit !

• v

C

( ∞ ) = x

= V

T

= V

A

• For t > 0, the switch is opened → τ = R

2

C

• v

C

( t ) = V

A

+ (

R

V

A

1

R

+ R

1

2

− V

A

) e

− t − t

0

R

2

C

→ V

A

• i

C

( t ) = C dv

C dt

( t )

= −

R

1

2

(

V

A

R

1

R

+ R

1

2

− V

A

) e

− t − t

0

R

2

C

→ 0

• After finding v

C

( t ), i

C

( t ), v

L

( t ), i

L

( t ), how can we find the remaining voltages or currents ?

• By substitution . i.e. Replace the capacitor/inductor by a voltage and/or current source with the found solution.

6

+

− v i

C i v

+ v

− i

• Here v ( t ) = v

C

( t ), i ( t ) = i

C

( t ), which are already found.

+

− v i

C i v

• Here v ( t ) = v

L

( t ), i ( t ) = i

L

( t ), which are already found.

+ v

− i

7

• Example :

4 A 1

1

2

1 F

+ vC

− vT

R

T

1 F

+ v C

1

4 A

1

2

1

1 io

2

+ voC =vT

Req = R

T

• R

T

= 1 Ω, By current division ⇒ i

0

= 1

4

4 = 1 A ⇒ v oc

= v

T

= 2 V

• τ = R

T

C = 1 sec , v

C

( ∞ ) = v

T

= 2 V . Assume that v

C

(0) = 1 V .

• v

C

( t ) − v

C

( ∞ ) = ( v

C

(0) − v

C

( ∞ )) e t − t

0

τ

• ⇒ v

C

( t ) = 2 − e − t ⇒ i

C

( t ) = C dv

C dt

( t )

= e − t

• Suppose that we want to find out, say, i

1 and v

2

.

⇒ Use substitution.

+ v2

+ i1

1

4 A 1 2 vC

• Here, v

C

= 2 − e − t . Simple node analysis yields :

• i

1

( t ) = 3 − 0 .

5 e − t , v

2

( t ) = 1 + 0 .

5 e − t .

8

• Example :

2 A

2 H i

L

1

2

1

2 A

1

2

1 iN

1

2

1

Req=R

T iN R

T i

L

2 H

• R

T

= 1 Ω, By KCL ⇒ 2 = v

1

+ i

N

, i

N

= v

1

⇒ i

N

= 1 A .

• τ = G

T

L = 2 sec , i

L

( ∞ ) = i

N

= 1 A . Assume that i

L

(0) = 3 V .

• i

L

( t ) − i

L

( ∞ ) = ( i

L

(0) − i

L

( ∞ )) e t − t

0

τ

• ⇒ i

L

( t ) = 1 + e − t

2

⇒ v

L

( t ) = L di

L dt

( t )

= − 2 e − t

2

• Suppose that we want to find out, say, i

1 and i

2

.

⇒ Use substitution.

i

L i1

2 i2

2 A

1

1

• Here, i

L

= 1 + e − t

2

. Simple node analysis yields :

• i

1

( t ) = 1 − e − t

2

, i

2

( t ) = 1 + e − t

2

.

9

• Response to a Pulse : This will depend on the relation between τ and T : v(t)

+

R vC A v(t)

C

− t

T

0 < t < T t > T

A

R

C

+ vC

R

C

+ vC

• If T À τ , v

C

( T ) ' v

C

( ∞ ) = A . Otherwise, v

C

( T ) = v

C

( ∞ ) = A vC(t) vC(t)

A

A

T

Time Constant < < T t

• Example : R = 1 k Ω, C = 1 µF , A = 10 V , T = 10 ms , v

C

(0) = 0 V .

• ⇒ τ = RC = 1 ms << T

• 0 < t < 10 ⇒ v

C

( t ) = 10 − 10 e − t ⇒ v

C

(10) ' 10 V

• t > 10 ⇒ v

C

( t ) = 10 e − ( t − 10)

• Example : R = 10 k Ω, C = 1 µF , A = 10 V , T = 10 ms , v

C

(0) = 0 V .

• ⇒ τ = RC = 10 ms = T

• 0 < t < 10 ⇒ v

C

( t ) = 10 − 10 e − 0 .

1 t ⇒ v

C

(10) = 10 − 10 e − 1 = 6 .

32

• t > 10 ⇒ v

C

( t ) = 6 .

32 e − 0 .

1( t − 10)

10

T

Time Constant comparable with T t

• Sinusoidal Response of First Order RC / RL Circuits :

• Here, the source term in the Th´evenin/Norton equivalent circuit is sinusoidal.

• dx dt

+

1

τ x =

1

τ x

∞ x

= V

A cos ωt

• x ( t ) = x

N

( t ) + x

F

( t ) = Natural Response + Forced Response

• This is the same as SUPERPOSITION. Natural response is due to initial condition x (0) and is called ZERO INPUT RESPONSE. This is the solution of ODE when the source term is set to ZERO.

• Forced response is due to source term and is called ZERO STATE RE-

SPONSE. This is the solution of ODE when x (0) = 0.

• dx

N dt

+

1

τ x

N

= 0 dx

F dt

+

1

τ x

F

=

1

τ

V

A cos ωt x

N

( t ) = Ke − t

τ

• x

F

( t ) = V

F cos( ωt + φ ) = a cos ωt + b sin ωt

• a = V

F cos φ , b = − V

F sin φ

• ˙

F

( t ) = − aω sin ωt + bω cos ωt

• ( bω +

1

τ a ) cos ωt + ( − aω +

1

τ b ) sin ωt =

1

τ

V

A cos ωt

• ( bω +

1

τ a ) =

1

τ

V

A

( − aω +

1

τ b ) = 0

• Given τ, V

A and ω Find a and b ⇒ V

F and φ

11

• Example 7-12 , p. 307.

• Note that since the switch is open for a long time → v (0) = 0.

• For Th´evenin Equivalent circuit : R

T

= 4 k Ω k 4 k Ω = 2 k Ω

• v

T

= 0 .

5 v s

( t ) = 10 sin 1000 t → τ = 2 .

10 3 × 10 − 6 = 2 .

10 − 3 sec.

• x

N

( t ) = Ke − t

τ

= Ke − 500 t

• x

F

( t ) = V

F cos( ωt + φ ) = a cos ωt + b sin ωt

• ( bω +

1

τ a ) = 0 ( − aω +

1

τ b ) =

1

τ

V

A

ω = 1000 Hz.

• 1000 b + 500 a = 0 − 1000 a + 500 b = 5000 −→ a = − 4 , b = 2

• v ( t ) = Ke − 500 t − 4 cos 1000 t + 2 sin 1000 t

• v (0) = 0 = K − 4 −→ K = 4

• a = V

F cos φ = − 4 , b = − V

F sin φ = 2

• V

F

=

√ a 2 + b 2 = 4 .

47, tan φ = − 2 / − 4 −→ φ = − 153 deg.

• v ( t ) = 4 e − 500 t + 4 .

47 cos(1000 t − 153)

• Note that as t → ∞ , −→ v ( t ) → 4 .

47 cos(1000 t − 153)

• This is called Sinusoidal Steady State . We will find it directly in

Chp. 8 in a simple way → Phasor Analysis.

12

• Second Order Circuits : The circuits which contain total of two capacitor- inductor combination.

→ 2 capacitors, 2 inductors, or 1 capacitor+

1 inductor.

• Before considering the most general case, we will first consider two important cases : series and parallel RLC circuits.

• Series RLC circuits i C C

+ v

C

L i

L

+ v

L

R

T

+ v

R v

T

C

+ v

C

+ v

L

• KVL : v

T

= v

R

+ v

C

+ v

L

KCL : i

R

= i

C

= i

L

• From the first order case, we know that v

C and i

L are state variables

(i.e. variables of ODE)

• i

C

= C dv

C dt

= i

L

−→ dv

C dt

= i

L

/C (1)

• v

T

= R

T i

R

+ v

C

+ v

L

= Ri

L

+ v

C

+ L di

L dt

• di

L dt

= −

1

L v

C

R

L

T i

L

+

1

L v

T

(2)

• (1) and (2) are called state equations . They are first order coupled

ODE’s. They can be written in matrix form as :

13

• d dt

 v

C i

L

=

0 1 /C

− 1 /L − R

T

/L

  v

C i

L

+

0

1 /L

V

T

• General form : −→ ˙ = Ax + bu

(*)

• x :(vector) state variable, u : input, A : matrix, b : vector.

• Alternative form : Scalar second order equation. Differentiate (1), use

(1) and (2) to eliminate i

L

:

• ¨

C

+

R

T

L v ˙

C

+

1

LC v

C

=

1

LC v

T

(**)

• So we have to either solve (*) or (**). Since they are equivalent, they give the same result. Usually we are given v

C

(0) and i

L

(0).

• To solve (**), we need ˙

C

(0). This comes from (1) : v ˙

C

(0) = i

L

(0) /C

• Before finding the solution of (**), let us consider the other case :

14

• Parallel RLC circuits i

C

C i

L

L i

N i

R

R i

C

C i

L

L

• KCL : i

N

= i

R

+ i

C

+ i

L

, KVL : v

R

= v

C

= v

L

,

• From the first order case, we know that v

C and i

L are state variables

(i.e. variables of ODE)

• v

L

= L di dt

L = v

C

−→ i

˙

L

= v

C

/L (1)

• i

N

= Gv

R

+ C v ˙

C

+ i

L

= Gv

C

+ C v ˙

C

+ i

L

• v ˙

C

= − G/Cv

C

− 1 /Ci

L

+ 1 /Ci

N

(2)

• (1) and (2) are called state equations and can be written also as :

• d dt

 v

C i

L

=

− G/C − 1 /C

1 /L 0

  v

C i

L

+

1 /C

0

 i

N

(*)

• Alternative form : Scalar second order equation. Differentiate (1), use

(1) and (2) to eliminate v

C

:

15

• i

L

+

G

C i

˙

L

+

1

LC i

L

=

1

LC i

N

(**)

• So we have to either solve (*) or (**). Since they are equivalent, they give the same result. Usually we are given v

C

(0) and i

L

(0).

• To solve (**), we need ˙ i

L

(0). This comes from (1) : i

˙

L

(0) = v

C

(0) /L

• Solution = zero input response + zero state response.

• Zero Input Response ( v

T

= 0, i

N

= 0)

• ¨ + a x + bx = 0

• Series RLC : x = v

C

, a =

R

T

L

, b =

1

LC

• Parallel RLC : x = i

L

, a =

G

C

, b =

1

LC

• x (0) and ˙ (0) are given.

• Assume solution of the form x ( t ) = e st ⇒ ˙ ( t ) = se st ⇒ ¨ ( t ) = s 2 e st

• ⇒ ( s 2 + as + b ) e st = 0 −→ ( s 2 + as + b ) = 0

• This is called the characteristic polynomial of the circuit, here s could be real of complex.

16

• ( s 2 + as + b ) = 0 −→ roots are s

1 and s

2

• Roots can be found as : s

1 , 2

= ±

− a ±

2 a 2 − 4 b

• Case 1 : Distinct Roots, s

1

= s

2

• x ( t ) = K

1 e s

1 t + K

2 e s

2 t

• Here K

1 and K

2 are constants (real or complex) to be found from the initial conditions.

• x (0) = K

1

+ K

2

, ˙ (0) = s

1

K

1

+ s

2

K

2

• K

1

= s

2 x (0) − ˙ (0) s

2

− s

1

K

2

= s

1 x (0) − ˙ (0) s

1

− s

2

• These formulas are valid even if s

1 and s

2 are complex.

• What if the roots are complex ?

• s = s

1 s

2

= − α + β ⇒ K

1

K

2

= r/ 2 e − θ

• x ( t ) = K

1 e s

1 t + K

2 e s

2 t = K

1 e st K

1 e = 2 < ( K

1 e st )

• x ( t ) = 2 < (( r/ 2) e − αt +  ( βt − θ ) ) = re − αt cos( βt − θ )

• Need to find r and θ by using initial conditions.

17

• x ( t ) = re − αt cos( βt − θ )

• x (0) = r cos θ −→ ˙ (0) = − αr cos θ + βr sin θ

• r cos θ = x (0) −→ r sin θ =

˙ (0)+ αx (0)

β

• Alternatively we could find the solution as :

• x ( t ) = C

1 e − αt cos βt + C

2 e − αt sin βt

• x (0) = C

1

, ˙ (0) = − αC

1

+ βC

2

−→ C

2

=

˙ (0)+ αx (0)

β

• Case 2 : Repeated Roots, s

1

= s

2

= s

• x ( t ) = K

1 e st + K

2 te st

• x (0) = K

1

, ˙ (0) = sK

1

+ K

2

−→ K

2

= ˙ (0) − sx (0)

18

• Stability of solutions

• s

1

= s

2

−→ x

N

( t ) = K

1 e s

1 t + K

2 e s

2 t

• s

1

= s

2

= s −→ x

N

( t ) = K

1 e st + K

2 te st

• If < ( s i

) < 0 −→ x

N

( t ) → 0 as t → ∞ −→ Stable Case .

• In this case, if the independent sources are bounded −→ solutions are bounded.

• If < ( s i

) > 0 , or s

1

= s

2

≥ 0 −→ x

N

( t ) → ∞ as t → ∞ −→ Unstable

Case .

• In this case, solutions are unbounded.

• For practical reasons, we want stable systems .

• From geometrical point of view, the roots of characteristic polynomial are in the open left half of the complex plane in the stable case.

• We will do further classification for the stable case, as explained in the next example.

• Example 7-15 , p. 318.

• Consider a series RLC circuit with no independent sources. (Hence we find zero input response, i.e. only the natural response). Let C = 0 .

25 µF ,

L = 1 H , v

C

(0) = 15 V , i

L

(0) = 0 A . Find the solution for : (a) R = 8 .

5 k Ω,

(b) R = 4 k Ω, (c) : R = 1 k Ω.

19

• ¨

C

+

R

T

L v ˙

C

+

1

LC v

C

=

1

LC v

T

= 0 (**)

• Characteristic polynomial :

• ⇒ ( s 2 + as + b ) = 0 −→ a =

• Roots can be found as : s

1 , 2

=

R

T

L

, b =

1

LC

− a ±

2 a 2 − 4 b

• Case 1 : a =

R

L

T = 8500, b =

1

LC

= 4 .

10 6 ⇒ s

1

= − 500, s

2

= − 8000.

• Roots are negative ⇒ Stable case.

• v

C

( t ) = K

1 e − 500 t + K

2 e − 8000 t

• v

C

(0) = K

1

+ K

2

= 15.

• v ˙

C

(0) = i

L

(0) /C = 0 ⇒ − 500 K

1

− 8000 K

2

= 0

• ⇒ K

1

= 16 , K

2

= − 1 ⇒ v

C

( t ) = 16 e − 500 t − e − 8000 t V

• C dv

C dt

= i

L

= − 2 .

10 − 3 e − 500 t + 2 .

10 − 3 e − 8000 t A

• This is called Overdamped Case (i.e. two distinct real-negative roots)

Overdamped Case

6

5

4

3

2

1

0

0 0.1

0.2

0.3

0.4

0.5

t (sec.)

0.6

0.7

0.8

0.9

1

20

• Case 2 : a =

R

L

T = 4000, b =

1

LC

= 4 .

10 6 ⇒ s

1

= s

2

= − 2000.

• v

C

( t ) = K

1 e − 2000 t + K

2 te − 2000 t

• v

C

(0) = K

1

= 15,

• v ˙

C

(0) = i

L

(0) /C = 0 ⇒ − 2000 K

1

+ K

2

= 0 ⇒ K

2

= 30000

• v

C

( t ) = (15 + 30000 t ) e − 2000 t V

• C dv

C dt

= i

L

= 15 te − 2000 t A

• This is called Critically Damped Case (i.e. two repeated real-negative roots)

Critically Damped Case

7

6

5

4

3

2

1

0

0 0.1

0.2

0.3

0.4

0.5

t (sec.)

0.6

0.7

0.8

0.9

1

• Case 3 : a =

R

L

T = 1000, b =

1

LC

= 4 .

10 6 ⇒ s

1 , 2

= − 500 ±  500

15.

• α = 500 , β = 500

15

• v

C

( t ) = Ke − 500 t

= K

1 e − 500 t cos(500 cos(500

15 t + φ )

15 t ) + K

2 e − 500 t sin(500

15 t )

21

• v

C

(0) = 15 = K

1

• v ˙

C

(0) = i

L

(0) /C = 0 ⇒ − 500 K

1

+ 500

15 K

2

= 0 ⇒ K

2

=

15

• v

C

( t ) = 15 e − 500 t cos(500

15 t ) +

15 e − 500 t sin(500

15 t )

• K cos φ = K

1

= 15 , K sin φ = − K

2

= −

15

• K =

15 2 + 15 = 15 .

5 , tan φ = −

15 ⇒ φ = − 75 .

52 deg.= − 1 .

32 rad.

• v

C

( t ) = 15 .

5 e − 500 t

• = 15 .

5 e − 500 t cos(500

15 t − 1 .

32) (True notation) cos(500

15 t − 75 .

52) (False but acceptable)

• This is called Underdamped Case (i.e. two complex conjugate roots with negative real part)

Underdamped Case

1

0

−1

−2

−3

−4

−5

0

3

2

0.1

0.2

0.3

0.4

0.5

t (sec.)

0.6

0.7

0.8

0.9

1

• Here s = − α + β ; α determines the decay, and β determines the frequency.

22

Im s2 s1

Overdamped

Re

Im s1=s2=s

Critically Damped

Re b

−a

Underdamped

• Step Response

• In this case, the standard ODE becomes :

• ¨ ( t ) + a x ( t ) + bx ( t ) = A

• x ( t ) = x

N

( t ) + x

F

• x

N

( t ) is the natural response and can be found as before.

• x

F

= B −→ ¨

F x

F

= 0 ⇒ x

F

= A/b

• Example 7-19, p. 328 . Series RLC circuit with V

T

= 10 V , C =

0 .

5 µF , L = 2 H , R = 1 k Ω, v

C

(0) = 0, i

L

(0) = 0.

• ¨

C

+

R

T

L v ˙

C

+

1

LC v

C

=

1

LC v

T

• ¨

C

( t ) + 500 ˙

C

( t ) + 10 6 v

C

( t ) = 10 7

(**)

23

• For x

N

, the characteristic polynomial is : s 2 + 500 s + 10 6 = 0

• Roots : s

1 , 2

= − 250 ±  968 −→ Underdamped case.

• v

CN

( t ) = K

1 e − 250 t cos 968 t + K

2 e − 250 t sin 968 t = Ke − 250 t cos(968 t + φ )

• V

CF

= 10 7 / 10 6 = 10

• v

C

( t ) = 10 + K

1 e − 250 t cos 968 t + K

2 e − 250 t sin 968 t

• v

C

(0) = 10 + K

1

= 0 −→ K

1

= − 10

• v ˙

C

(0) = i

L

(0) /C = 0 ⇒ − 250 K

1

+ 968 K

2

= 0 −→ K

2

= − 2 .

58

• v

C

( t ) = 10 − 10 e − 250 t cos 968 t − 2 .

58 e − 250 t sin 968 t

• K cos φ = K

1

= − 10 , K sin φ = − K

2

= 2 .

58

• K =

100 + 2 .

58 2 = 10 .

12, φ = 104 .

46 deg.

• The characteristic polynomial can also be written as :

• s 2 + 2 ξω

0 s + ω 2

0

= 0

• ξ : damping ratio, ω

0

: undamped natural frequency.

• s

1 , 2

= ω

0

( − ξ ±

ξ 2 − 1)

• ξ > 1 −→ Overdamped Case.

• ξ = 1 −→ Critically damped Case.

• 0 < ξ < 1 −→ Underdamped case.

• ξ = 0 −→ Lossless Case. In this case, the natural response is a pure sinusoid .

24

• General Second Order Circuits

• Note that we have v

C and i

L as variables, and by element relations we have i

C

= C v ˙

C and v

L

= L

˙ i

L

.

• Hence the general strategy is as follows :

• Step 1 : Use any method we have seen (node, mesh, combined constraints etc.) to obtain i

C and v

L in terms of v

C

, i

L and independent sources only. (This is a process of writing equations, and eliminating undesired variables ⇒ Linear Algebra)

• At the end of step 1 , we obtain the following equations :

• i

C

= c

11 v

C

+ c

12 i

L

+ d

1 u

1

• v

L

= c

21 v

C

+ c

22 i

L

+ d

2 u

2

• Here, coefficients c ij

, d i depend on circuit parameters, u i depend on independent sources.

• Step 2 : Use i

C

= C v ˙

C and v

L

= L i

˙

L

:

• C v ˙

C

= c

11 v

C

+ c

12 i

L

+ d

1 u

1

• L i

˙

L

= c

21 v

C

+ c

22 i

L

+ d

2 u

2

• These equations can be written either in component form :

• v ˙

C

= a

11 v

C

+ a

12 i

L

+ b

1 u

1

(*)

˙ i

L

= a

21 v

C

+ a

22 i

L

+ b

2 u

2

(**)

• Or in matrix form :

25

• d dt

 v

C i

L

=

 a

11 a

21 a

12 a

22

  v

C i

L

+

 b

1 u

1 b

2 u

2

• General form : −→ ˙ = Ax + bu

(*)

• x :(vector) state variable, u : input, A : matrix, b : vector or matrix.

• Alternative form : Scalar second order equation. Differentiate ( ∗ ) or

( ∗∗ ), use these equations to eliminate i

L or v

C

:

• Case 1 : a

12

= 0

• ¨

C

= a

11 v ˙

C

+ a

12 i

˙

L

+ b

1 u

1

= a

11 v ˙

C

+ a

12

( a

21 v

C

+ a

22 i

L

+ b

2 u

2

) + b

1 u

1

• = a

11 v ˙

C

+ a

12 a

21 v

C

+ a

22 a

12 i

L

+ a

12 b

2 u

2

+ b

1 u

1

• = a

11 v ˙

C

+ a

12 a

21 v

C

+ a

22

( ˙

C

− a

11 v

C

− b

1 u

1

) + a

12 b

2 u

2

+ b

1

˙

1

• = ( a

11

+ a

22 C

+ ( a

12 a

21

− a

11 a

22

) v

C

− a

22 b

1 u

1

+ a

12 b

2 u

2

+ b

1 u

1

• ¨

C

− ( a

11

+ a

22

) ˙

C

+ ( a

11 a

22

− a

12 a

21

) v

C

= − a

22 b

1 u

1

+ a

12 b

2 u

2

+ b

1

˙

1

• Case 2 : a

21

= 0. Change v

C with i

L and indexes 1 ←→ 2, we obtain :

• i

L

− ( a

22

+ a

11

)˙ i

L

+ ( a

22 a

11

− a

21 a

12

) i

L

= − a

11 b

2 u

2

+ a

21 b

1 u

1

+ b

2 u

2

• Let us see the relation with A :

• ( a

11

+ a

22

) = Trace( A ) = T

• ( a

11 a

22

− a

12 a

21

) = det A = D

• ¨ − T ˙ + Dx = u s

• v

C

Case : u s

= − a

22 b

1 u

1

+ a

12 b

2 u

2

+ b

1 u

1

• i

L

Case : u s

= − a

11 b

2 u

2

+ a

21 b

1 u

1

+ b

2

˙

2

26

v s

R1

+ v

C1

R2

C1

+ v

C2

C2

• KCL at C

1

: i

C 1

+ G

1

( v

C 1

− v s

) + G

2

( v

C 1

− v

C 2

) = 0

• ⇒ C

1 v ˙

C 1

= − ( G

1

+ G

2

) v

C 1

+ G

2 v

C 2

+ G

1 v s

• KCL at C

2

: i

C 2

+ G

2

( v

C 2

− v

C 1

) = 0

• ⇒ C

2 v ˙

C 2

= G

2 v

C 1

− G

2 v

C 2

• ⇒ a

11

= − ( G

1

+ G

2

) /C

1

, a

12

= G

2

/C

1

, a

21

= G

2

/C

2

, a

22

= − G

2

/C

2

, b

1

= G

1

/C

1

, u

1

= v s

, b

2

= 0, u

2

= 0

• ( a

11

+ a

22

) = Trace( A ) = T = − (( G

1

+ G

2

) /C

1

+ G

2

/C

2

)

• ( a

11 a

22

− a

12 a

21

) = det A = D = G

1

G

2

/C

1

C

2

• By using Case 2 : u s

= − a

11 b

2 u

2

+ a

21 b

1 u

1

+ b

2 u

2

= ( G

1

G

2

/C

1

C

2

) v s

• ¨

C 2

+ (( G

1

+ G

2

) /C

1

+ G

2

/C

2 v

C 2

+ ( G

1

G

2

/C

1

C

2

) v

C 2

= ( G

1

G

2

/C

1

C

2

) v s

• Given initial conditions v

C 1

(0) and v

C 2 the second state equation given above : v

C 2

(0) from

• ⇒ C

2 v ˙

C 2

(0) = G

2 v

C 1

(0) − G

2 v

C 2

(0)

• Given the parameters G i

, R i and the source term v s

, we can solve this

ODE to find v

C 2

.

• Then we can find ˙

C 2 by differentiation. By using the second equation, we can find v

C 1

...etc...

27

• Example on p. 334 , Fig. 7-14

+ v

C1 v s

R1

+ v

1

R2

+ v

2

C1

C2

+

+ v o

• KCL for Node 1 : i

C 1

+ G

1

( v

1

− v s

) + G

2

( v

1

− v

2

) = 0

• KCL for Node 2 : i

C 2

+ G

2

( v

2

− v

1

) = 0

• Op-amp eqn : v

2

= v

+

= v

= v o

−→ v

C 1

= v

1

− v o

= v

1

− v

2

, v

C 2

= v

2

• C

1 v ˙

1

= C

1 v ˙

1

− C

1 v ˙

2

= − ( G

1

+ G

2

) v

1

+ G

2 v

2

+ G

2 v s

• C

2 v ˙

2

= G

2 v

1

− G

2 v

2

• v ˙

2

= ( G

2

/C

2

) v

1

− ( G

2

/C

2

) v

2

• C

1 v ˙

1

= C

1

( G

2

/C

2

) v

1

− C

1

( G

2

/C

2

) v

2

− ( G

1

+ G

2

) v

1

+ G

2 v

2

+ G

2 v s

• v ˙

1

= ( G

2

/C

2

− (( G

1

+ G

2

) C

1

) ) v

1

+ ( ( G

2

/C

1

) − ( G

2

/C

2

)) v

2

+ ( G

2

/C

1

) v s

• applying Case 2, we obtain :

• ¨

2

+ (( G

1

+ G

2

) /C

1 2

+ ( G

1

G

2

/C

1

C

2

) v

2

= ( G

1

G

2

/C

1

C

2

) v s

• As before, given the parameters, and the initial conditions, we can solve this ODE. Then, we can find v

1

. Then we can find all of the remaining voltages and currents ...etc...

28

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