SS 20. For the unity-feedback system in Figure P9.1, withdo the following:G (s) =K(s+4) (s+6) (s +10)a. Design a controller that will yield no more than 25% overshootand no more than a 2-second settling time for a step input andzero steady-state error for step and ramp inputs.MATLABb.MLUse MATLAB and verify your design.SS21. Redo Problem 20 using Octave in the following way:Octave will ask for the desired percent overshoot, settling time and PI compensator zero from the user.i) Design the PD controller's zero and display the root locus of the PID-compensated system with thedesired percent overshoot line.ii) Display the gain and the transient response characteristics of the PID-compensated systemiii) Display the step response of the systemiv) Display the ramp response of the system

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Answered: SS 20. For the unity-feedback system in…

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

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Can you also please do the simulate the step response in MATLAB for the design and report archieved PO and settling time? Thank you.
Can you also please do the simulate the step response in MATLAB for the design and report achieved PO and settling time? Thank you.
Please solve the following WITHOUT the use of AI. Do not run the prompt through chatgpt. Using MATLAB for the required question, solve the problems. Thank you!
DO NOT COPY SOLUTION- will report The differential equation of a cruise control system is provided by the following equation: Find the closed loop transfer function with respect to the reference velocity (vr) . a. Find the poles of the closed loop transfer function for different values of K. How does the poles move as you change K? b. Find the step response for different values of K and plot in MATLAB. What can you observe?
1) Consider the system below: Vehicle Controller Steering dynamics Desired Actual bearing angle bearing angle 50 1 K s2 + 10s + 50 s(s + 5) Figure 1: Simplified Block Diagram of a Self-Guiding Vehicle's Bearing Angle Control. • Find a K value that the system has minimum rise time and minimum overshoot. Let us call this proportional gain as Kopt Show each step while finding Kopt- Show the necessary graphical solutions. Simulate the system response with 3 different K values. (Kopt and two other K values close to Kopt) Show the system response (actual bearing angle) in a single graph for different K values. • Comment on the results.
DO NOT COPY SOLUTION The differential equation of a cruise control system is provided by the following equation: Find the closed loop transfer function with respect to the reference velocity (vr) . a. Find the poles of the closed loop transfer function for different values of K. How does the poles move as you change K? b. Find the step response for different values of K and plot in MATLAB. What can you observe? c. For the given transfer function, find tp, ts, tr, Mp . Plot the resulting step response. G(s) = 40/(s^2 + 4s + 40)
Please solve the following by hand and without the use of AI. Thank you!
1. (Without Octave) Design a controller (C) to have A) a zero steady-state error B) less than 20% overshoot 1 с s + 10 2. Discuss whether you can design a controller, having requirement at question 1 as well as 0.1 second settling time. 3. F(s) = = 1 s(s+1) Find angle of F(s) at the point s = -2+j2. 4. Given a unity feedback system that has the forward transfer function G(s) = - K s s² + 4s +8 a) Calculate the angle of G(s) at the point (-3+j0) by finding the algebraic sum of angles of the vectors drawn from the zeros and poles of G(s) to the given point. b) Determine if the point specified in a) is on the root locus. c) If the point specified in a) is on the root locus, find the gain, K, using the lengths of vectors.
The differential equation of a cruise control system is provided by the following equation: WRITE OUT SOLUTION DO NOT USE A COPIED SOLUTION Find the closed loop transfer function with respect to the reference velocity (vr) . a. Find the poles of the closed loop transfer function for different values of K. How does the poles move as you change K? b. Find the step response for different values of K and plot in MATLAB. What can you observe?
please explain step by step
Q5) For unity feedback control system with forward transfer function (G(s) ): G(s) = ; By using root locus graph calculate the value K(s+5) (s+2)(s²+12s+50) of gain (K) which must be added to get the dominant root at damping ratio (-0.886) and natural frequency (w = 8 rad/sec )? www CTRICAL ENGIN
Hi, I could use some help with the following problems for controls. I am trying to get this to work, but I keep getting stuck. I'm trying to review some problems for an upcoming test by using some online resources.

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