Step Input MCQ Quiz in தமிழ் - Objective Question with Answer for Step Input - இலவச PDF ஐப் பதிவிறக்கவும்

Last updated on Mar 26, 2025

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Latest Step Input MCQ Objective Questions

Top Step Input MCQ Objective Questions

Step Input Question 1:

The open loop transfer function of a control system with unity negative feedback is given by G(s)=5(2+4s)(1+9s)(4+3s)

The steady state error, due to unit step input is _______

Answer (Detailed Solution Below) 0.28 - 0.29

Step Input Question 1 Detailed Solution

G(s)=5(2+4s)(1+9s)(4+3s)

For step input, steady state error is given by

Ess=A1+Kp

Kp=its0G(s)=its05(2+4s)(1+9s)(4+3s)=104=2.5

Ess=11+2.5=13.5=0.286

Step Input Question 2:

In the given system, find the steady state error due to step disturbance D(s).

FT 7+AFT 2 file 1 (19 Q) images Q13

  1. 11000
  2. 11000
  3. 1100
  4. 1100

Answer (Detailed Solution Below)

Option 2 : 11000

Step Input Question 2 Detailed Solution

The simplified system rearranged to show disturbance as input and error or output is:

FT 7+AFT 2 file 1 (19 Q) images Q13a

eD()=lims0sG2(s)D(s)1+G1(s)G2(s) 

For step input D(s)=1s

eD()=lims011G1(s)lims0G(s) 

=11000 

Step Input Question 3:

The closed loop frequency response |M(jω)|-vs- frequency of a second order system is shown. The steady-state error due to step input is ____.

GATE EC FT 5 10

Answer (Detailed Solution Below) 0.1

Step Input Question 3 Detailed Solution

Steady-state error will occur when the output variation reaches a steady state, i.e. step output.

∴ The steady-state error is calculated at ω = 0.

|M| = 0.9 → steady-state value of unit step response

ess = 1 – 0.9

= 0.1

Step Input Question 4:

The Block diagram of a control system is shown

Control System FT2 images q3

Value of K1 such that steady state error due to step input is zero is

Answer (Detailed Solution Below) 1

Step Input Question 4 Detailed Solution

solving 1st loop

Control System FT2 images q3a

G1(s)=1s+31+K3s+3

G1(s)=1s+3+k3

Step 2

(1s+3+k3)(1s+1)

(1s2+(4+k3)s+(3+k3))

Step 3 = Solving 2nd loop

G(s)=1s3+(4+k3)s2(3+k3+k2)s

H(s) = K1

CLTF=1s3+(4+k3)s2+(3+k3+k2)s+k1

For Non-unity feedback system

e(t) = r(t) – y(t)

e(t)=r(t)[1y(t)r(t)]

Laplace domain

E(s)=SR(s)[1Y(s)R(s)]

E(s) = SR(s) [1 - CLTF]

For steady state error

S → 0

ess=lims×1s[11s3+(4+k3)s2+(3+k2+k3)s+k1]

= 0

= 1 – K1 = 0

K1 = 1

Step Input Question 5:

If the steady state error of the system shown below to unit step input is zero. Then the DC gain of the feedback network H(s) is ______.

Control Systems (3,  4 and 5) images Q2

Answer (Detailed Solution Below) 0.5

Step Input Question 5 Detailed Solution

Concept:

Error = input – output

e(t) = r(t) – c(t)

taking replace

e(s)=lts0s[R(s)C(s)] 

E(s)=lts0sR(s)[1C(s)R(s)] 

E(s)=lts0sR(s)[1CLTF] 

Application:

E(s)=lts0s×1s[14s+21+(4s+2)H(s)]=0 

=lts0[14s+2s+2+4H(s)s+2]=0 

=lts04s+2+4H(s)=0 

4=2+4lts0H(s) 

24=lts0H(s) 

lts0H(s)=12 

= DC gain of feedback path

Step Input Question 6:

A system is shown in the given figure. The value of k which gives a steady state error of 20% to a unit step input is given by

GATE IN Control systems 1 madhu images Q15

  1. 500
  2. 100
  3. 20
  4. 4

Answer (Detailed Solution Below)

Option 4 : 4

Step Input Question 6 Detailed Solution

Concept:

The Steady-state error for different types of system is as shown:

Type of System

Step Input

Ramp Input

Parabolic Input

Type-0

A1+Kp

Type-1

0

AKv

Type-2

0

0

AKa

 

Where ‘Kp, Kv, and Ka are the system gain.

Calculation:

G(s)H(s)=k(1+s)(1+4s)

Since this is a type-zero system, the steady-state error will be:

ess=11+Kp

Kp=limsG(s)

Kp=limsk(1+s)(1+4s)=k

ess=11+Kp=0.2

11+K=0.2

K = 4

Step Input Question 7:

A system is described by the following state matrices A=[0248],B=[02],C=[22]. Then the steady state error for unit step input is

  1. 0.5
  2. 1
  3. 0

Answer (Detailed Solution Below)

Option 4 : 0

Step Input Question 7 Detailed Solution

Closed loop transfer function,

 T(s)=G(s)H(s)1+G(s)H(s)=C[sIA]1B

Now, we have

(sIA)=[s24s+8]

(sIA)1=1(s2+8s+8)[s+824s]

(sIA)1B=1(s2+8s+8)[s+824s][02]=1(s2+8s+8)[42s]

C[sIA1]B=1(s2+8s+8)[22][42s]=4(s+2)(s2+8s+8)

Open loop transfer function =G(s)H(s)=T(s)1T(s)=4(s+2)(s2+8s+8)4(s+2)

=4(s+2)s2+4s

=4(s+2)s(s+4)

∴ Position error constant Kp=lims0G(s)H(s)=

∴ Steady state error =ess=11+Kp=0

Note:

For step input, steady state error ess=[1+C(A1)B]

For ramp input, steady rate error ess=limt[[1+C(A1)B]t+C(A1)2B]

Step Input Question 8:

The Block Diagram of a system is shown below. The steady state error for TL(s)=1s is { Assume that R(s)=0}

19070

  1. 0.2

  2. 1.2

  3. 5

  4. 6

Answer (Detailed Solution Below)

Option 1 :

0.2

Step Input Question 8 Detailed Solution

When reference input is zero i.e. R(s)=0, the transfer function between C(s) and TL(s) is given by

C(s)TL(s)=10.15s2+s1+50.15s2+s=10.15s2+s+5C(s)=10.15s2+s+5(1s)

We know error E(s)=R(s)C(s)

E(s)=0C(s)=10.15s2+s+51s

The steady state error due to TL is given by

ess=1ts0s.E(s)=1ts0s10.15s2+s+51s=10+0+5=0.2ess=0.2

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