Question 4 (a) A feedback control system with a proportional controller is shown in Figure Q4...
Q.4 A position control system is shown in Figure Q4. Assume that K(s) = K, the plant 50 s(0.2s +1) transfer function is given by G(s) s02s y(t) r(t) Figure Q4: Feedback control system. (a) Design a lead compensator so that the closed-loop system satisfies the following specifications (i) The steady-state error to a unit-ramp input is less than 1/200 (ii) The unit-step response has an overshoot of less than 16% Ts +1 Hint: Compensator, Dc(s)=aTs+ 1, wm-T (18 marks)...
Automatic Control In unity feedback system with Gs) (s-IXs-2) With out controller, is this system stable, and why? For Gc K (proportional control) sketch the root locus. Find the range of K to make the system stable. Determine the range of K, so that the system has no overshoot Determine the range of K for steady state error to unit step input less than 20% a) b) c) d) e) In unity feedback system with Gs) (s-IXs-2) With out controller,...
PROBLEM 4 Suppose that a system is shown in Figure 4. There are three controllers that might be incorporated into this system. 1. Ge (s)-K (proportional (P) controller) 2. GS)K/s (integral (I) controller) 3. G (s)K(1+1/s) (proportional, integral (PI) controller) The system requirements are T, < 10 seconds and P0 10% for a unit step response. (a) For the (P) controller, write a piece of MATLAB code to plot root locus for 0<K<,and find the K value so that the...
Consider a unity-feedback control system with a PI controller Gpr(s) and a plant G(s) in cascade. In particular, the plant transfer function is given as 2. G(s) = s+4, and the PI controller transfer function is of the forrm KI p and Ki are the proportional and integral controller gains, respectively where K Design numerical values for Kp and Ki such that the closed-loop control system has a step- response settling time T, 0.5 seconds with a damping ratio of...
Please solve as a MATLAB code. A unity feedback closed loop control system is displayed in Figure 4. (a) Assume that the controller is given by G (s) 2. Based on the lsim function of MATLAB, calculate and obtain the graph of the response for (t) at. Here a 0.5°/s. Find the height error after 10 seconds, (b) In order to reduce the steady-state error, substitute G (s) with the following controller This is a Proportional-Integral (PI) controller. Repeat part...
10. Consider the system shown in Figure 1. Assuming a second-order system approximation, design the following controllers based on the root locus shown in Figure 2 o esign a gain adjustment controller Co) -K such that the damping ratio amping ratio ζ = 0.5 Design a lag compern 348+pe such that the steady-state error under a step ensator C(s) input ess is 1o of that in the case of gain adjustment with K 64 s + Pe Figure 1: System...
Question 3 (10 +10+10+15 45 marks) E(s) C(s) R(s) Figure 3: Unity feedback control system for Question 3 For the unity feedback control system shown in Figure 3, 100 G(S) (s+2)(+10) Page 3 of 7 NEE3201 Examination Paper CRICOS Provider No: 00124k a) Determine the phase margin, the gain crossover frequency, the gain margin, the phase crossover frequency of the system when Gc(s)-1, 10 marks) b) Design a proportional controller Gc(s)-K so that a phase margin of 50° is achieved....
Q4 For the following Proportional controller use the step response and root locus rules obtain the root locus schematics for positive gain. (30 pts) Rs) ー10 a. Find the gain and frequency for marginal stability b. Find the gain for critical damping c. Find the real part and the gain ofthe CL pole for a =4 d. Find K that provides the system with 8 dB gain margin and find the complex poles for that gain e. Find the phase...
Q1. Show analytically that the Root Locus for the unity feedback system with open loop transfer function: (a) [10 marks] K(s 4) (s + 2) is a circle, and find the centre and the radius. Determine the minimum value of the damping ratio and the corresponding value of K (b) The root locus of the open loop transfer function: [10 marks] s(s26s +15) is depicted in Figure Q1(b). Find the minimum value of gain K that will render the system...
2a. Determine a proper controller so that the feedback control system below will have the damping ratio of < = 0.7 and the natural frequency of n = 10.0 rad/sec. Your choices are: Proportional controller, K Lead controller, 17, a < 1 Lag controller, v a > 1 Proportional + Derivative controller, K (1 + Tas) Proportional + Integral + Derivative controller, K(1+1/(Ts) + Tas) Or Lead Lag controller If the resulting feedback control system has an order greater than...