The forward-route transfer function is applied to the input of a negative unit feedback system as at the bottom, and the overrun rate is given as %OS=8.9% at the exit of the K 27- G(s) = system. (s + 1)? What is the system's stable state error in this case? account for it. O A) 0.41 OB) 0.3 OC) 0.37 OD) 0.32

The forward-route transfer function is applied to the input of a negative unit feedback system as at the bottom, and the overrun rate is given as %OS=8.9% at the exit of the K 27- G(s) = system. (s + 1)? What is the system's stable state error in this case? account for it. O A) 0.41 OB) 0.3 OC) 0.37 OD) 0.32

Introductory Circuit Analysis (13th Edition)

13th Edition

ISBN:9780133923605

Author:Robert L. Boylestad

Publisher:Robert L. Boylestad

Chapter1: Introduction

Section: Chapter Questions

Problem 1P: Visit your local library (at school or home) and describe the extent to which it provides literature...

See similar textbooks

Similar questions

The forward transfer function G(s) with a H(s) feedback configuration of an uncompensated Basic Satellite Launching System is as shown in figures 1 and 2. A- Write a m-script and generate the time and frequency response of the system shown in Figure 1. (a = 4, b = 2, c=2, d = 1and e=10, and f=4). B- Compute the percent overshoot, peak time and settling time, using second order approximation through pole zero cancellation and unity feedback configuration shown in figure 2.
When a unit ramp input is applied to the unity feedback system having closed loop transfer function, C(s)/R(s)= Ks+b/s2+as+b , (a>0, b>0, K>0), the steady state error will be ?
are given a system’s transfer function as T(s) = 21 Construct a state-space model for the given system using ” Observer Canonical Form” method. | that the full state information of this system is available, design a state-feedback controller for this put the desired closed loop poles at ~2+ 2. Now, assume that the state information of the system are measurable, for this case what kind of controller do you suggest? Design this controller so that the ¢ Joop poles of the system are located at —10 + 510.
What should K be for a negative unit feedback system to be marginally stable, given the open transfer loop function? a- K=0.2 b- K≥2 c- K=8 d- K≥8 e-none
For a negative unity feedback system, using Routh-Hurwitz criterion for stability, determine the value of K for which the system is marginally stable.
For a negative unity feedback system with the given forward transfer function:1. Evaluate the system type, Kp, Kv, and Ka.2. What is the value of the position constant?3. What is the value of the velocity constant?4. What is the value of the acceleration constant?5. What is the amount of steady-state error if the system received a parabolic function signal?
Consider the feedback system given the open loop transfer function below G(s)H(s) = K / ( S (s+3) (s+2)) a) Using the Routh-Hurwitz criterion, for which value of K, the poles of the closed-loop system take the pure imaginary value.b) What will be the maximum value of K for the system to be stable?c) Calculate the value of K, where the real value of the complex root of the system is Re{s}=-1. Tip 1: Closed loop transfer function T(s) = G(s) / ( 1+ G(s)H(s)) .Routh HurwitzIn order to perform the criterion analysis, the denominator of the closed-loop function will be examined. Tip 2: The real value of the system complex root Re{s}=-1 is expressed by the following formula f^2(s) = p(s-1) p(s) is the payoff of the closed-loop function.
a : for the unity feedback system G(s)=k/s(s+n). determine k and n such that the response for the input R(s)=1 has form: c(t)=(co+cit)eª ?and evaluate c, and c, when all initial condition are zero? Q3 b: for a unity feedback system G(s)=2/s(s+3) ,determine Ess when the input equal to: 1. Step 2. Ramp 3. parabolic
A unity feedback system has loop transfer function: L(s) = Gc(s)G(s) = 4(s+z)/s(s+1)(s+3) a) Draw root locus as z varries from 0 to100 b) using root locus, estimate the percentage overshoot and settling time (within 2%) of system at z =4 c) determine actual overshoot and settling time at z = 4
For the system of Figure 2, ? = 2 s and?(?) =?(? + 0.8)(? − 1)(? − 0.6)Figure 2. Unity feedback system.a) Determine the range of ? for stability using the Routh–Hurwitz criterion.b) Determine the range of ? for stability using the Jury test. For more detailed question you can look at the image.
Consider the unity feedback system shown below. Determine the range of values of K for which the system is stable by using Routh-Hurwitz method. Find the critical value of K and oscillation frequency.
Given a unity feedback system, what value of K will result to steady state error of 8%?