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 aninput 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 inputgiven in (a)?s(1/s²)e(00) = Cramp (00) = lim1+G(s)105+sG(s)= lim1lim sG(s)5-0

Answered: Image /qna-images/answer/c7eb40a7-2b28-414b-9bd5-49e1f5472a24.jpg

Answered: P.4: R(s) + E(s) K(s+7)…

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

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)
Solve the initial value problem. y" + 4y' + 20y = 0: y(0) = 2 y (0) = - 3 %3D Chapter 6, Section 6.2, Go Tutorial Problem 12 Find Y(s). 2s + 5 Y(s): s2 + 4s + 20 2s + 5 Y(s) = s2 + 4s + 20 2s – 5 Y(s) : + 4s + 20 2 + 4s + 20 Y(s) 2s + 5
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
Response using matlab.
Consider the following Initial Value Problem (IVP) dy /at = -t * sin (y); y(t = 0) =1 Solve for y(t=0.5) using a) Forward Euler method with At = 0.25. (Solve by hand) Develop a Matlab script that solves for y (t = 5) using Forward Euler method. Use the time step levels given below and plot t vs y in the same plot. Include the plot with the right format (axis labels, legends, ...) in your solution sheet and include your Matlab script in the solution as well. i) At = 0.25 ii) At = 0.125 b) Backward Euler method with At = 0.25 (Solve by hand)
3. Using the trial function uh(x) = a sin(x) and weighting function wh(x) = b sin(x) find an approximate solution to the following boundary value problems by determining the value of coefficient a. For each one, also find the exact solution using Matlab and plot the exact and approximate solutions. (One point each for: (i) finding a, (ii) finding the exact solution, and (iii) plotting the solution) a. (U₁xx - 2 = 0 u(0) = 0 u(1) = 0 b. Modify the trial function and find an approximation for the following boundary value problem. (Hint: you will need to add an extra term to the function to make it satisfy the boundary conditions.) (U₁xx - 2 = 0 u(0) = 1 u(1) = 0
/Simulate to solve the following ordinary differential equation by using Simulink tool box and represent the output result. x(t)= sin(3t) = 3x(t) + 1-2y dt
A mechanical system is represented by two masses and three springs, where m, = 12 kg, m, = 22kg, and spring constants k, = k, = k, = 15 N/m, as shown in the following figure. k3 m2 Determine the largest eigenvalue of this mechanical system using the characteristic equation. a. b. Determine the smallest eigenvalue and the corresponding eigenvector using Inverse Power method. Given the initial eigenvector v(0)= (1 1 1). Iterate until | Ar41 - 1x 50.0005.
The eigenvectors (v), and (v), of the following system: 6.0000 0.0000 (0.0000 4.0000 87.0000 -56.0000 (x))+ -56.0000 56.0000 {x(t)} 0 are, 0.7592 -0.7932 1.0000 1.0000 0.9784 1.0000 1.0000 -0.9784 0.2265 -0.2366 1.0000 1.0000 1.2049 -1.2587 1.0000 1.0000
Given the trasnfer function G(s) numerator and denominator coefficients for Matlab code should be: O s³+2s+1 2s4+2s²+1' the num= [1 0 2 1] and den=[2 020 1] O num=[1 2 1] and den=[2 0 2 1 1] O num=[1 2 1] and den=[2 2 1] O num=[1 0 2 1] and den=[2 2 0 1]
P.3: An input of 25t³u(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(co) = lim- 01+G(s) C(s)
! 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).

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