P.3: An input of 25t³u(t) applied to the input of a Type 3 unity feedbacksystemwhere210(s+4)(s+6)(s+11)(s +13)$³ (s+7)(s+ 14)(s +19)G(s) =Find the steady-state error in position.R(s) +E(s)G(s)SR(s)e(co) = lim-01+G(s)C(s)

Answered: Image /qna-images/answer/9203adab-ab6a-4f9a-9381-79eb2712759e.jpg

Answered: P.3: An input of 251³u(t) applied to…

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

See similar textbooks

Similar questions

2- Using Matlab, what are the step response curves of the closed-loop system, as shown in fig.1. the feedback represents the second-order dynamic system. (fill in the following table) For=0.4 Wn 1 3 6 9 10 R(S) 0.1 0.3 0.6 0.9 1 For w 5 rad/sec 3 Settling time Peak response 2 Wn s(s+23wn) Settling time Peak response C(s) Discuss the follow Which parameters or w occur on the rise time of the response? Which parameter increases the speed of response? Which parameters can be decreases the response amplitude? Which parameter decreases the steady error state? fig.2
P.4: R(s) + E(s) K(s+7) s(s+5)(5 + 8)(5 + 12) C(s) a. What value of K will yield a steady-state error in position of 0.01 for an input of (1/10)? b. What is the K, for the value of K found in (a)? c. What is the minimum possible steady-state position error for the input given in (a)? s(1/s²) e(00) = Cramp (00) = lim1+G(s) 1 05+sG(s) = lim 1 lim sG(s) 5-0
Feedback & Control Systems State-Space Representation Write the state-space representation of the system below. Let the output of the mechanical system is x3 (t). 1 N-s/m x₁ (t) M3 = 1kg 1 N/m М1 -0000 1kg > X3 (t) 1 N-s/m 1 N/m oooo x₂ (t) M₂ 1kg 4 1 N-s/m² -1 N-s/m →f(t)
6. Given the system shown below, design a value of K so that for an input of 100tu(t), there will be a 0.01 steady-state error. R(s) K s(s + 1) 10s K C(s)
Q4) A particular control system yielded a steady state error of 0.20 for unit step input. A unit integrator is cascaded to this system and unit ramp input is applied to this modified system. What is the value of steady-state error for this modified system?
100(s+2)(s+5) s(s+8)(s+12) evaluate the static ) For the control system with the transfer function (s) %3D error constants and find the expected steady state errors for the standard step, ramp and parabolic inputs. * Using a well labeled diagram show the following specifications i. delay time ii. peak overshoot 前。 settling time iv. rise time CENIOR
Required information Use the following transfer functions to find the steady-state response yss() to the given input function f(t). NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. T(-) Y(s) F(s) s(e) 10 b. = 9 sin 2t s²(s+1) ' The steady-state response for the given function is yss() = | sin(2t + 2.0344).
The Routh-Hurwitz criterion to be used to determine the stability of a system with a characteristic equation given by 85 + 2s4 + 2s3 + 4s² + 11s + 10 Comment on the stability of the system. Neutral Stable Unstable
Q\1 Sketch root locus for the systems below, find k-range for stability, sd. and k at zeta 0.5. k 1. G(s) = H(s): = 1 $65²+5s+7)
! a. Required information Use the following transfer functions to find the steady-state response yss(t) to the given input function f(t). NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. T(s) Y(s) 6 f(t) F(s) s(s²+10s+100) ⁹ The steady-state response for the given function is yss(t) = = = = 6 sin 9t sin(9t-2.93).
7. What is the response to unit step function input when all initial conditions are zero. R + 2 S(S + 3) a) C(t) = 1 + 2e-t +e-2t b) C(t) = 1 – 2e-t + e2t c) C(t) = 1 – et + 2e-2t d) C(t) = 1 – 2e t + e-2t
1 Problem 5 4 State, x(t) SAWNO-Nw. ● ● Case 1 O 2 6 Time, sec. underdamped critically damped State, x(t) • overdamped 54321 ONS TY Case 2 2 ▷ Time, sec. 8 10 State, x(t) 5 2 + 3 4 Case 3 2 ▷ 6 Time, sec. 5432 State, x(t) & A & No. 2 Match each of the resposes above to one of the following second-order system types: • undamped Case 4 ▷ Time, sec.

SEE MORE QUESTIONS

Recommended textbooks for you

Elements Of Electromagnetics

Mechanical Engineering

ISBN:

9780190698614

Author:

Sadiku, Matthew N. O.

Publisher:

Oxford University Press

Mechanics of Materials (10th Edition)

Mechanical Engineering

ISBN:

9780134319650

Author:

Russell C. Hibbeler

Publisher:

PEARSON

Thermodynamics: An Engineering Approach

Mechanical Engineering

ISBN:

9781259822674

Author:

Yunus A. Cengel Dr., Michael A. Boles

Publisher:

McGraw-Hill Education

Elements Of Electromagnetics

Mechanical Engineering

ISBN:

9780190698614

Author:

Sadiku, Matthew N. O.

Publisher:

Oxford University Press

Mechanics of Materials (10th Edition)

Mechanical Engineering

ISBN:

9780134319650

Author:

Russell C. Hibbeler

Publisher:

PEARSON

Thermodynamics: An Engineering Approach

Mechanical Engineering

ISBN:

9781259822674

Author:

Yunus A. Cengel Dr., Michael A. Boles

Publisher:

McGraw-Hill Education

Control Systems Engineering

Mechanical Engineering

ISBN:

9781118170519

Author:

Norman S. Nise

Publisher:

WILEY

Mechanics of Materials (MindTap Course List)

Mechanical Engineering

ISBN:

9781337093347

Author:

Barry J. Goodno, James M. Gere

Publisher:

Cengage Learning

Engineering Mechanics: Statics

Mechanical Engineering

ISBN:

9781118807330

Author:

James L. Meriam, L. G. Kraige, J. N. Bolton

Publisher:

WILEY

SEE MORE TEXTBOOKS

P.3: An input of 251³u(t) applied to the input of a Type 3 unity feedback system where 210(s+4)(s+6)(s+11)(s +13) $³ (s+7)(s+14)(s +19) G(s) = Find the steady-state error in position. R(s) + E(s) G(s) SR(s) e(00) = lim+G(s) C(s)