s -3 +4i s 4+3i 1+0.707 1 b) What is the gain, K, associated with that point? Ans: Problem 3: A system is characteri...
If the initial cone A E Re has a root locus plot started in Figure P1. Determine the following about the root locus determine a) the transfer f a) Of points A, B & C indicated on the real axis which are on the root locus? Ans b) the DC gain of b) How many zeros are there at infinity? Ans c) What angles do the infinity zero asymptote(s) make with the positive real axis? Ans d) Where do the...
Please explain every step as clearly and detailed as possible. B Frequency Response Modeling Frequency response modeling of a linear system is based on the premise that the dynamics of a linear system can be recovered from a knowledge of how the system responds to sinusoidal inputs. (This will be made mathematically precise in Theorem 13.) In other words, to determine (or iden- tify) a linear system, all one has to do is observe how the system reacts to sinusoidal...
50 400 Problem 3: A system has the transfer function: G(s) -8s+24s +800 3+80 Assuming time for this system is expressed in seconds,if the system is subjected to a periodic input of 4 sin cot, determine: a) The frequency o where the amplitude of the output will be at its maximum. b) The functional expression for how the output amplitude varies with the input frequency, o. c) The functional expression for how the phase of the output with respect to...
1. Consider the unity feedback system shown in figure 1 with G(S) -2sti a) Determine the closed loop transfer function TF(s) γ(s) R(s) What are the poles and zeros of TF1(s)? [2 marks] b) For TF(s), calculate the DC gain, natural frequency and damping ratio. Classify TF1(s) as underdamped overdamped, critically damped or undamped [3 marks] c) Use the initial value theorem and final value theorem to determine the initial value (Mo) and final value (M) of the [2 marks]...
1. Consider the system shown. Assume B-3 N-s/m and K-7 N/m. Negligible Mass a) Find the transfer function, H(s)-X(s)Fa(s) b) Using the transfer function, find the unit step response and the unit impulse response. c) Using the transfer function, find the steady-state response when fa(t) 2 sin (4t) d) Find the free response (zero-input response) assuming x(0) 2 m.
3. (28 pts.) The unity feedback system with K(5+3) G(s) = (s + 1)(s + 4)(s + 10) is operating with 12% overshoot ({=0.56). (a) the root locus plot is below, find the settling time (b) find ko (c) using frequency response techniques, design a lead compensator that will yield a twofold improvement in K, and a twofold reduction in settling time while keeping the overshoot at 12%; the Bode plot is below using the margin command and using the...
The parameters are as follows k=10 a=0.50 b=0.3 c=0.6 d=9 w_1=12 w_2=15 Kv=30 A feedback control system (illustrated in Figure 1) needs to be designed such that the closed-loop system is asymptotically stable and such that the following design criteria are met: the gain crossover frequency wc should be between w1 and w2. the steady-state error should be zero in response to a unit step reference. the velocity constant should be greater than Kv (in other words, the steady-state unit...
The parameters are as follows k=10 a=0.50 b=0.3 c=0.6 d=9 w_1=12 w_2=15 Kv=30 A feedback control system (illustrated in Figure 1) needs to be designed such that the closed-loop system is asymptotically stable and such that the following design criteria are met: the gain crossover frequency wc should be between w1 and w2. the steady-state error should be zero in response to a unit step reference. the velocity constant should be greater than Kv (in other words, the steady-state unit...
e c(s) X(s) S+3 B(s) D(s) Kh PROBLEM 1 Consider the system shown in the figure above. Write an expression for signal.Xs) in terms of complex variable s and output signal C(s). a) b) Write the closed-loop transfer fiunction C( for the system. for the system. ) Recalling that for a second-order system such as this, that the closed-loop transfer function has the form damping ratio ?= 0.5 and an undamped natural frequency on-6 rads. T , determine the values...
The parameters are as follows k=0.1,a=1.00,b=1,c=1.0,d=25,w_1=20,w_2=25,Kv=50 e(t) r(t) e (t) G(s) Figure 1: Feedback control system A pulley and belt transmission has a linearized relationship between the driven pulley angle e (t) in degrees and the input torque u(t) in Newton meters given by the following differential equation du(t) dt A feedback control system (illustrated in Figure 1) needs to be designed such that the closed-loop system is asymptotically stable and such that the following design criteria are met 1....