Control systems engineering norman nise, Exercises of Linear Control Systems

linear control asdas sa dasdsa

Typology: Exercises

2020/2021

Uploaded on 04/13/2021

hamzsohail9
hamzsohail9 🇨🇭

5

(4)

1 document

1 / 53

Toggle sidebar

This page cannot be seen from the preview

Don't miss anything!

bg1
E1SM 11/11/2010 9:29:8 Page 1
Solutions to Skill-Assessment
Exercises
CHAPTER 2
2.1
The Laplace transform of tis 1
s2using Table 2.1, Item 3. Using Table 2.2, Item 4,
FsðÞ¼ 1
sþ5ðÞ
2.
2.2
Expanding F(s) by partial fractions yields:
FsðÞ¼A
sþB
sþ2þC
sþ3ðÞ
2þD
sþ3ðÞ
where,
A¼10
sþ2ðÞsþ3ðÞ
2S!0¼5
9B¼10
ssþ3ðÞ
2S!2¼5
C¼10
ssþ2ðÞ
S!3¼10
3;and D¼sþ3ðÞ
2dF sðÞ
ds s!3¼40
9
Taking the inverse Laplace transform yields,
ftðÞ¼5
95e2tþ10
3te3tþ40
9e3t
2.3
Taking the Laplace transform of the differential equation assuming zero initial
conditions yields:
s3CsðÞþ3s2CsðÞþ7sC sðÞþ5CsðÞ¼s2RsðÞþ4sR sðÞþ3RsðÞ
Collecting terms,
s3þ3s2þ7sþ5

CsðÞ¼ s2þ4sþ3

RsðÞ
Thus,
CsðÞ
RsðÞ¼s2þ4sþ3
s3þ3s2þ7sþ5
1
pf3
pf4
pf5
pf8
pf9
pfa
pfd
pfe
pff
pf12
pf13
pf14
pf15
pf16
pf17
pf18
pf19
pf1a
pf1b
pf1c
pf1d
pf1e
pf1f
pf20
pf21
pf22
pf23
pf24
pf25
pf26
pf27
pf28
pf29
pf2a
pf2b
pf2c
pf2d
pf2e
pf2f
pf30
pf31
pf32
pf33
pf34
pf35

Partial preview of the text

Download Control systems engineering norman nise and more Exercises Linear Control Systems in PDF only on Docsity!

Solutions to Skill-Assessment

Exercises

CHAPTER 2

The Laplace transform of t is

s 2

using Table 2.1, Item 3. Using Table 2.2, Item 4,

F sð Þ ¼

ð s þ 5 Þ

2

Expanding F(s) by partial fractions yields:

F sð Þ ¼

A

s

þ

B

s þ 2

þ

C

ðs þ 3 Þ

2

þ

D

ðs þ 3 Þ

where,

A ¼

ð s þ 2 Þ ðs þ 3 Þ

2 S! 0

B ¼

s sð þ 3 Þ

2 S! 2

C ¼

s sð þ 2 Þ S! 3

; and D ¼ ðs þ 3 Þ

2 dF sð Þ

ds s! 3

Taking the inverse Laplace transform yields,

f tð Þ ¼

 5 e

 2 t þ

te

 3 t þ

e

 3 t

Taking the Laplace transform of the differential equation assuming zero initial

conditions yields:

s

3 C sð Þ þ 3 s

2 C sð Þ þ 7 sC sð Þ þ 5 C sð Þ ¼ s

2 R sð Þ þ 4 sR sð Þ þ 3 R sð Þ

Collecting terms,

s

3 þ 3 s

2 þ 7 s þ 5

C sð Þ ¼ s

2 þ 4 s þ 3

R sð Þ

Thus,

C sð Þ

R sð Þ

s

2 þ 4 s þ 3

s^3 þ 3 s^2 þ 7 s þ 5

G sð Þ ¼

C sð Þ

R sð Þ

2 s þ 1

s 2 þ 6 s þ 2

Cross multiplying yields,

d

2 c

dt 2

þ 6

dc

dt

þ 2 c ¼ 2

dr

dt

þ r

C sð Þ ¼ R sð ÞG sð Þ ¼

s 2

s

ðs þ 4 Þ ðs þ 8 Þ

s sð þ 4 Þ ðs þ 8 Þ

A

s

þ

B

ðs þ 4 Þ

þ

C

ðs þ 8 Þ

where

A ¼

ð s þ 4 Þ ðs þ 8 Þ S! 0

B ¼

s sð þ 8 Þ S! 4

; and C ¼

s sð þ 4 Þ S! 8

Thus,

c tð Þ ¼

e

 4 t þ

e

 8 t

Mesh Analysis

Transforming the network yields,

V(s)

I 1 (s) I 2 (s)

V 1 (s)

V 2 (s)

I 9 (s)

(^1 )

s s

s

_

_

Now, writing the mesh equations,

ð s þ 1 ÞI 1 ð Þ s sI 2 ð Þ s I 3 ð Þ ¼s V sð Þ

sI 1 ð Þ þs ð 2 s þ 1 ÞI 2 ð Þ s I 3 ð Þ ¼s 0

I 1 ð Þ s I 2 ð Þ þs ðs þ 2 ÞI 3 ð Þ ¼s 0

Solving the mesh equations for I 2 (s),

I 2 ð Þ ¼s

ð s þ 1 Þ V sð Þ  1

s 0  1

 1 0 ð s þ 2 Þ

ð s þ 1 Þ s  1

s ð 2 s þ 1 Þ  1

 1  1 ðs þ 2 Þ

s

2 þ 2 s þ 1

V sð Þ

s s 2 ð þ 5 s þ 2 Þ

2 Solutions to Skill-Assessment Exercises

Solving for X 2 (s),

X 2 ð Þ ¼s

s

2 þ 3 s þ 1

F sð Þ

 ð 3 s þ 1 Þ 0

s

2 þ 3 s þ 1

 ð 3 s þ 1 Þ

 ð 3 s þ 1 Þ s

2 þ 4 s þ 1

ð 3 s þ 1 ÞF sð Þ

s s 3 þ 7 s 2 ð þ 5 s þ 1 Þ

Hence,

X 2 ð Þs

F sð Þ

ð 3 s þ 1 Þ

s s 3 þ 7 s 2 ð þ 5 s þ 1 Þ

Writing the equations of motion,

s

2 þ s þ 1

u 1 ð Þ s ðs þ 1 Þu 2 ð Þ ¼s T sð Þ

 ðs þ 1 Þu 1 ð Þ þs ð 2 s þ 2 Þu 2 ð Þ ¼s 0

where u 1 ð Þs is the angular displacement of the inertia.

Solving for u 2 ð Þs,

u 2 ð Þ ¼s

s 2 þ s þ 1

T sð Þ

 ðs þ 1 Þ 0

s

2 þ s þ 1

 ðs þ 1 Þ

 ðs þ 1 Þ ð 2 s þ 2 Þ

ðs þ 1 ÞF sð Þ

2 s 3 þ 3 s 2 þ 2 s þ 1

From which, after simplification,

u 2 ð Þ ¼s

2 s 2 þ s þ 1

Transforming the network to one without gears by reflecting the 4 N-m/rad spring to

the left and multiplying by (25/50)

2 , we obtain,

Writing the equations of motion,

s

2 þ s

u 1 ð Þ s sua ð Þ ¼s T sð Þ

su 1 ð Þ þs ðs þ 1 Þua ð Þ ¼s 0

where u 1 ð Þs is the angular displacement of the 1-kg inertia.

Solving for ua ð Þs,

ua ð Þ ¼s

s

2 þ s

T sð Þ

s 0

s

2 þ s

s

s ðs þ 1 Þ

sT sð Þ

s 3 þ s 2 þ s

4 Solutions to Skill-Assessment Exercises

From which,

ua ð Þs

T sð Þ

s^2 þ s þ 1

But, u 2 ð Þ ¼s

ua ð Þs:

Thus,

u 2 ð Þs

T sð Þ

s 2 þ s þ 1

First find the mechanical constants.

Jm ¼ Ja þ JL

2

¼ 1 þ 400

Dm ¼ D (^) a þ DL

2

¼ 5 þ 800

Now find the electrical constants. From the torque-speed equation, set vm ¼ 0 to

find stall torque and set T (^) m ¼ 0 to find no-load speed. Hence,

T (^) stall ¼ 200

vnoload ¼ 25

which,

K (^) t

R (^) a

T (^) stall

Ea

K (^) b ¼

E (^) a

vnoload

Substituting all values into the motor transfer function,

um ð Þs

Ea ð Þ s

K T

R (^) a J (^) m

s s þ

J (^) m

Dm þ

K (^) T K (^) b

R (^) a

s s þ

where um ð Þs is the angular displacement of the armature.

Now uL ð Þ ¼s

um ð Þs. Thus,

uL ð Þs

Ea ð Þ s

s s þ

Letting

u 1 ð Þ ¼s v 1 ð Þs=s

u 2 ð Þ ¼s v 2 ð Þs=s

Chapter 2 Solutions to Skill-Assessment Exercises (^5)

Solving for e v (^) oþdv ,

e

v (^) oþdv ¼ e

v (^) o þ

de

v

dv v (^) o

dv ¼ e

vo þ e

v (^) o dv

Substituting into Eq. (1)

ddv

dt

þ e

vo þ e

v (^) o dv  2 ¼ i tð Þ ð^2 Þ

Setting i tð Þ ¼ 0 and letting the circuit reach steady state, the capacitor acts like an

open circuit. Thus, v (^) o ¼ v (^) r with ir ¼ 2. But, ir ¼ e

v (^) r or v (^) r ¼ lni (^) r.

Hence, v (^) o ¼ ln 2 ¼ 0 :693. Substituting this value of v (^) o into Eq. (2) yields

ddv

dt

þ 2 dv ¼ i tð Þ

Taking the Laplace transform,

ð s þ 2 Þdv sð Þ ¼ I sð Þ

Solving for the transfer function, we obtain

dv sð Þ

I sð Þ

s þ 2

or

V sð Þ

I sð Þ

s þ 2

about equilibrium:

CHAPTER 3

Identifying appropriate variables on the circuit yields

C 1

iL i^ C 2

iC 1

i (^) R

C 2

R

L v 1 (t) v (^) o(t)

Writing the derivative relations

C 1

dv (^) C 1

dt

¼ iC 1

L

di (^) L

dt

¼ v (^) L

C 2

dv (^) C 2

dt

¼ iC 2

ð 1 Þ

Chapter 3 Solutions to Skill-Assessment Exercises (^7)

Using Kirchhoff’s current and voltage laws,

i (^) C 1 ¼ iL þ i (^) R ¼ iL þ

R

v (^) L  v (^) C 2 ð Þ

v (^) L ¼ v (^) C 1 þ v (^) i

i (^) C 2 ¼ iR ¼

R

v (^) L  v (^) C 2 ð Þ

Substituting these relationships into Eqs. (1) and simplifying yields the state

equations as

dv (^) C 1

dt

RC 1

v (^) C 1 þ

C 1

i (^) L 

RC 1

v (^) C 2 þ

RC 1

v (^) i

di (^) L

dt

L

v (^) C 1 þ

L

v (^) i

dv (^) C 2

dt

RC 2

v (^) C 1

RC 2

v (^) C 2

RC 2

v (^) i

where the output equation is

v (^) o ¼ v (^) C 2

Putting the equations in vector-matrix form,

x^ _ ¼

RC 1

C 1

RC 1

L

RC 2

RC 2

x þ

RC 1

L

RC 2

v (^) i ð Þt

y ¼ ½ 0 0 1 Šx

Writing the equations of motion

s 2 þ s þ 1

X 1 ð Þs sX 2 ð Þs ¼ F sð Þ

sX 1 ð Þ þs s 2 þ s þ 1

X 2 ð Þs X 3 ð Þs ¼ 0

X 2 ð Þ þs s

2 þ s þ 1

X 3 ð Þ ¼s 0

Taking the inverse Laplace transform and simplifying,

x € 1 ¼  x_ 1  x 1 þ x_ 2 þ f

x € 2 ¼ x_ 1  x_ 2  x 2 þ x 3

x € 3 ¼  x_ 3  x 3 þ x 2

Defining state variables, z (^) i,

z 1 ¼ x 1 ; z 2 ¼ x_ 1 ; z 3 ¼ x 2 ; z 4 ¼ x_ 2 ; z 5 ¼ x 3 ; z 6 ¼ x_ 3

8 Solutions to Skill-Assessment Exercises

The state equation is converted to a transfer function using

G sð Þ ¼ C ðs I  AÞ

 1 B ð^1 Þ

where

A ¼

; B ¼

; and C ¼ ½ 1 : 5 0 : 625 Š:

Evaluating ðs I  AÞ yields

ð s I  AÞ ¼

s þ 4 1 : 5

 4 s

Taking the inverse we obtain

ð s I  AÞ

 1 ¼

s 2 þ 4 s þ 6

s  1 : 5

4 s þ 4

Substituting all expressions into Eq. (1) yields

G sð Þ ¼

3 s þ 5

s^2 þ 4 s þ 6

Writing the differential equation we obtain

d

2 x

dt 2

þ 2 x

2 ¼ 10 þ df tð Þ ð^1 Þ

Letting x ¼ x (^) o þ dx and substituting into Eq. (1) yields

d

2 ðx (^) o þ dxÞ

dt 2

þ 2 ðx (^) o þ dxÞ

2 ¼ 10 þ df tð Þ ð^2 Þ

Now, linearize x

2 .

ð x (^) o þ dxÞ

2  x

2 o

d x

2

dx x (^) o

dx ¼ 2 x (^) odx

from which

ð x (^) o þ dxÞ

2 ¼ x

2 o þ^2 x^ odx^ ð 3 Þ

Substituting Eq. (3) into Eq. (1) and performing the indicated differentiation gives

us the linearized intermediate differential equation,

d

2 dx

dt 2

þ 4 x (^) odx ¼  2 x

2 o þ 10 þ df tð Þ ð^4 Þ

The force of the spring at equilibrium is 10 N. Thus, since F ¼ 2 x

2 ; 10 ¼ 2 x

2 o from

which

x (^) o ¼

ffiffiffi 5

p

10 Solutions to Skill-Assessment Exercises

Substituting this value of x (^) o into Eq. (4) gives us the final linearized differential

equation.

d

2 dx

dt 2

þ 4

ffiffiffi 5

p dx ¼ df tð Þ

Selecting the state variables,

x 1 ¼ dx

x 2 ¼ d_x

Writing the state and output equations

x _ 1 ¼ x 2

x _ 2 ¼€dx ¼  4

ffiffiffi 5

p x 1 þ df tð Þ

y ¼ x 1

Converting to vector-matrix form yields the final result as

x _ ¼

ffiffiffi 5

p 0

x þ

df tð Þ

y ¼ ½ 1 0 Šx

CHAPTER 4

For a step input

C sð Þ ¼

10 ðs þ 4 Þ ðs þ 6 Þ

s sð þ 1 Þ ðs þ 7 Þ ðs þ 8 Þ ðs þ 10 Þ

A

s

þ

B

s þ 1

þ

C

s þ 7

þ

D

s þ 8

þ

E

s þ 10

Taking the inverse Laplace transform,

c tð Þ ¼ A þ Be

t þ Ce

 7 t þ De

 8 t þ Ee

 10 t

Since a ¼ 50 ; T (^) c ¼

a

¼ 0 :02s; T (^) s ¼

a

¼ 0 :08 s; and

T (^) r ¼

a

¼ 0 :044 s.

a. Since poles are at  6  j 19 : 08 ; c tð Þ ¼ A þ Be  6 t cos 19ð : 08 t þ fÞ.

b. Since poles are at  78 :54 and  11 : 46 ; c tð Þ ¼ A þ Be  78 : 54 t þ Ce  11 : 4 t .

c. Since poles are double on the real axis at  15 c tð Þ ¼ A þ Be  15 t þ Cte  15 t :

d. Since poles are at j 25 ; c tð Þ ¼ A þ B cos 25ð t þ fÞ.

a. (^) v n ¼^

ffiffiffiffiffiffiffiffi 400

p ¼ 20 and 2zvn ¼ 12 ; ;z ¼ 0 :3 and system is underdamped.

b. (^) vn ¼

ffiffiffiffiffiffiffiffi 900

p ¼ 30 and 2zvn ¼ 90 ; ;z ¼ 1 :5 and system is overdamped.

c. (^) vn ¼

ffiffiffiffiffiffiffiffi 225

p ¼ 15 and 2zvn ¼ 30 ; ;z ¼ 1 and system is critically damped.

d. (^) vn ¼

ffiffiffiffiffiffiffiffi 625

p ¼ 25 and 2zvn ¼ 0 ; ;z ¼ 0 and system is undamped.

Chapter 4 Solutions to Skill-Assessment Exercises (^11)

b. Since F ðt  tÞ ¼

e

 ðt tÞ 

e

 4 ðt tÞ 2

3

e

 ðt tÞ 

e

 4 ðt tÞ

e

 ðt tÞ þ

e

 4 ðt tÞ 

e

 ðt tÞ þ

e

 4 ðt tÞ

and

Bu ð Þ ¼t

e  2 t

; F ðt  tÞBu ð Þ ¼t

e

t e

t 

e

2 t e

 4 t

e

t e

t þ

e

2 t e

 4 t

Thus, x ð Þ ¼t F ð Þtx ð Þ þ 0

R

t 0

F ðt  tÞ

BU ð Þtdt ¼

e

t  e

 2 t 

e

 4 t

e

t þ e

 2 t þ

e

 4 t

c. y tð Þ ¼ ½ 2 1 Šx ¼ 5 e

t  e

 2 t

CHAPTER 5

Combine the parallel blocks in the forward path. Then, push

s

to the left past the

pickoff point.

1

s

s

s

s

s 2

1

R ( s ) C ( s )

Combine the parallel feedback paths and get 2s. Then, apply the feedback formula,

simplify, and get, T sð Þ ¼

s 3 þ 1

2 s 4 þ s 2 þ 2 s

Find the closed-loop transfer function, T sð Þ ¼

G sð Þ

1 þ G sð ÞH sð Þ

s 2 þ as þ 16

, where

and G sð Þ ¼

s sð þ aÞ

and H sð Þ ¼ 1. Thus, vn ¼ 4 and 2zvn ¼ a, from which z ¼

a

But, for 5% overshoot, z ¼

ln

ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi

p 2 þ ln

s ¼ 0 :69. Since, z ¼

a

; a ¼ 5 :52.

Chapter 5 Solutions to Skill-Assessment Exercises (^13)

Label nodes.

R ( s )

s

s N 1 ( s ) N 2 ( s ) N 3 ( s ) N 4 ( s )

N 5 ( s ) N 6 ( s )

N 7 ( s )

s

C ( s )

1 s

1 s

Draw nodes.

R ( s ) N 1 ( s )^ N 2 ( s )

N 5 ( s )

N 7 ( s )

N 6 ( s )

N 3 ( s ) N 4 ( s ) (^) C ( s )

Connect nodes and label subsystems.

R ( s ) 1 C ( s )

1 s

s

− 1

s^ s

(^1 )

− 1

1

1 s N 1 ( s ) N 2 ( s )

N 5 ( s ) N 6 ( s )

N 7 ( s )

N 3 ( s ) (^) N 4 ( s )

Eliminate unnecessary nodes.

R ( s ) (^1) s s C ( s )

1 s

1 s

  • s

14 Solutions to Skill-Assessment Exercises

Writing the state equations from the signal-flow diagram, we obtain

x ¼

x þ

r

y ¼ ½ 100 500 Šx

From the transformation equations,

P

 1 ¼

Taking the inverse,

P ¼

Now,

P

 1 AP ¼

P

 1 B ¼

CP ¼ ½ 1 4 Š

Therefore,

_z ¼

z þ

u

y ¼ ½ 0 : 8  1 : 4 Šz

First find the eigenvalues.

jlI  Aj ¼

l 0

0 l

l  1  3

4 l þ 6

¼ l

2 þ 5 l þ 6

From which the eigenvalues are 2 and 3.

Now use Ax (^) i ¼ lx (^) i for each eigenvalue, l.

Thus,

x 1

x 2

¼ l

x 1

x 2

For l ¼ 2,

3 x 1 þ 3 x 2 ¼ 0

 4 x 1  4 x 2 ¼ 0

16 Solutions to Skill-Assessment Exercises

Thus x 1 ¼ x 2

For l ¼  3

4 x 1 þ 3 x 2 ¼ 0

 4 x 1  3 x 2 ¼ 0

Thus x 1 ¼ x 2 and x 1 ¼  0 : 75 x 2 ; from which we let

P ¼

Taking the inverse yields

P

 1 ¼

Hence,

D ¼ P

 1 AP ¼

P

 1 B ¼

CP ¼ ½ 1 4 Š

Finally,

z _ ¼

z þ

u

y ¼ ½  2 : 121 2 : 6 Šz

CHAPTER 6

Make a Routh table.

s

7 3 6 7 2

s

6 9 4 8 6

s 5 4.666666667 4.333333333 0 0

s

4 4.35714286 8 6 0

s

3 12.90163934 6.426229508 0 0

s

2 10.17026684 6 0 0

s

1 1.18515742 0 0 0

s

0 6 0 0 0

Since there are four sign changes and no complete row of zeros, there are four right

half-plane poles and three left half-plane poles.

Make a Routh table. We encounter a row of zeros on the s

3 row. The even polynomial

is contained in the previous row as  6 s 4 þ 0 s 2 þ 6. Taking the derivative yields

Chapter 6 Solutions to Skill-Assessment Exercises (^17)

CHAPTER 7

a. First check stability.

T sð Þ ¼

G sð Þ

1 þ G sð Þ

10 s

2 þ 500 s þ 6000

s 3 þ 70 s 2 þ 1375 s þ 6000

10 ðs þ 30 Þ ðs þ 20 Þ

ð s þ 26 : 03 Þ ðs þ 37 : 89 Þ ðs þ 6 : 085 Þ

Poles are in the lhp. Therefore, the system is stable. Stability also could be checked

via Routh-Hurwitz using the denominator of T(s). Thus,

15 u tð Þ : e (^) step ð 1 Þ ¼

1 þ lim s! 0

G sð Þ

1 þ 1

15 tu tð Þ : e (^) ramp ð 1 Þ ¼

lim s! 0

sG sð Þ

 20

 30

 35

15 t

2 u tð Þ : e (^) parabola ð 1 Þ ¼

lim s! 0

s

2 G sð Þ

¼ 1; since L 15 t

2 ¼

s 3

b. First check stability.

T sð Þ ¼

G sð Þ

1 þ G sð Þ

10 s

2 þ 500 s þ 6000

s 5 þ 110 s 4 þ 3875 s 3 þ 4 : 37 e 04 s 2 þ 500 s þ 6000

10 ðs þ 30 Þ ðs þ 20 Þ

ð s þ 50 : 01 Þ ðs þ 35 Þ ðs þ 25 Þ s 2 ð  7 : 189 e  04 s þ 0 : 1372 Þ

From the second-order term in the denominator, we see that the system is unstable.

Instability could also be determined using the Routh-Hurwitz criteria on the

denominator of T(s). Since the system is unstable, calculations about steady-state

error cannot be made.

a. The system is stable, since

T sð Þ ¼

G sð Þ

1 þ G sð Þ

1000 ðs þ 8 Þ

ð s þ 9 Þ ðs þ 7 Þ þ 1000 ðs þ 8 Þ

1000 ðs þ 8 Þ

s 2 þ 1016 s þ 8063

and is of Type 0. Therefore,

K (^) p ¼ lim s! 0

G sð Þ ¼

 8

 9

¼ 127 ; K (^) v ¼ lim s! 0

sG sð Þ ¼ 0 ;

and K (^) a ¼ lim s! 0

s

2 G sð Þ ¼ 0

b.

estep ð 1 Þ ¼

1 þ lim s! 0

G sð Þ

1 þ 127

¼ 7 : 8 e  03

e (^) ramp ð 1 Þ ¼

lim s! 0

sG sð Þ

e (^) parabola ð 1 Þ ¼

lim s! 0

s

2 G sð Þ

Chapter 7 Solutions to Skill-Assessment Exercises (^19)

System is stable for positive K. System is Type 0. Therefore, for a step input

e (^) step ð 1 Þ ¼

1 þ K (^) p

¼ 0 :1. Solving for Kp yields K (^) p ¼ 9 ¼ lim s! 0

G sð Þ ¼

12 K

 18

; from

which we obtain K ¼ 189.

System is stable. Since G 1 ð Þ ¼s 1000, and G 2 ð Þ ¼s

ðs þ 2 Þ

ð s þ 4 Þ

e (^) D ð 1 Þ ¼ 

lim s! 0

G 2 ð Þ s

þ lim G 1 s! 0

ð Þ s

2 þ 1000

¼  9 : 98 e  04

System is stable. Create a unity-feedback system, where H (^) e ð Þ ¼s

s þ 1

s

s þ 1

The system is as follows:

R ( s ) E^ a ( s )^100 C ( s )

s + 4

s

s + 1

Thus,

G (^) e ð Þ ¼s

G sð Þ

1 þ G Sð ÞH (^) e ð Þ s

ð s þ 4 Þ

100 s

ðs þ 1 Þ ðs þ 4 Þ

100 ðs þ 1 Þ

S

2  95 s þ 4

Hence, the system is Type 0. Evaluating Kp yields

K (^) p ¼

The steady-state error is given by

e (^) step ð 1 Þ ¼

1 þ K (^) p

1 þ 25

¼ 3 : 846 e  02

Since G sð Þ ¼

K sð þ 7 Þ

s 2 þ 2 s þ 10

; e ð 1 Þ ¼

1 þ K (^) p

1 þ

7 K

10 þ 7 K

Calculating the sensitivity, we get

S (^) e:K ¼

K

e

@e

@K

K

10 þ 7 K

ð 10 Þ 7

ð 10 þ 7 KÞ

2

7 K

10 þ 7 K

20 Solutions to Skill-Assessment Exercises