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Consider the root loous shown for the system Gs) i. What is K for a system...
Q.10- For the system shown in Figure 5 with K (s + 3)(s +5) Gs)s-2)s-4) Find the range of gain, K, which will cause the system to be stable. Cs) Q.11. Draw the Root Locus of the following systems...
Q.10- For the system shown in Figure 5 with K (s + 3)(s +5) Gs)s-2)s-4) Find the range of gain, K, which will cause the system to be stable. Cs) Q.11. Draw the Root Locus of the following systems. Find the points of intersection with the real and imaginary axis. 6(s)H(s)- s(s +2) K(s+5) of- Draw the Bode diagram of the following tmamsfer finction. His)- -100 s +12s +21s +10 213- Obtain the phase and gain margins of the system...
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 contr...
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...
For the root locus shown below, find that makes s=-4 one of the closed loop system...
For the root locus shown below, find that makes s=-4 one of the closed loop system poles. Root Locus 15 10 Imaginary Axis (seconds) -10 -15 6 - 1 0 -3 -2 Real Axis (seconds)
Sketch the root locus for the control system shown in Figure Q3(b). b) Calculate the breakaway...
Sketch the root locus for the control system shown in Figure Q3(b). b) Calculate the breakaway value of K and its location. Comment on the stability of the system. 1 G(s) and Ge(s) K (s+ 1) (s+2) where K is a positive constant C(s) R(s) G(s) Ge(s) Figure Q3(b) If the control system is modified by an addition of an open loop pole at s - 6 ii) 1 sketch the new root locus showing such that G(s) (s+1) (s+2)(s...
A system having an open loop transfer function of G(S) = K10/(S+2)(3+1) has a root locus...
A system having an open loop transfer function of G(S) = K10/(S+2)(3+1) has a root locus plot as shown below. The location of the roots for a system gain of K= 0.248 is show on the plot. At this location the system has a damping factor of 0.708 and a settling time of 4/1.5 = 2.67 seconds. A lead compensator is to be used to improve the transient response. (Note that nothing is plotted on the graph except for that...
A plant with the transfer function Gp(s)-- with unity feedback has the root locus shown in the figure below: (s+2)(s+4) Root Locus 1.5 C(s) 0.5 0.5 1.5 .3 Real Axis (seconds) (a) Determine K of G...
A plant with the transfer function Gp(s)-- with unity feedback has the root locus shown in the figure below: (s+2)(s+4) Root Locus 1.5 C(s) 0.5 0.5 1.5 .3 Real Axis (seconds) (a) Determine K of Gp(s) if it is desired that the uncompensated system has a 10% OS (overshoot) to a step input. (4 points) a 5% overshoot and a peak time Tp 3.1 meets the requirements described in part (b) and achieves zero steady state (b) Compute the desired...
Please solve part b and c and d !! Consider the closed loop system shown in...
Please solve part b and c and d !!
Consider the closed loop system shown in Figure 4. The root locus of that system is shown in Figure 5 (s+40s+8) R(s) Y(s) Figure 4 System block diagram of Problem 4 a) On the root locus plot, sketch the region of possible roots of the dominant closed-loop poles such that the system response to a unit step has the following time domain specifications. [5] i. Damping ratio, 20.76 ii. Natural frequency,....
9. Consider a negative unity-feedback control system with the loop transfer function s +8 D(s) G(8)=K-...
9. Consider a negative unity-feedback control system with the loop transfer function s +8 D(s) G(8)=K- s+1) ((s + 1)2 + 22 (s + 94 + 793 + 1932 +33s + 20 (a) Determine the asymptotes of the root-locus diagram for K > 0, if any. (06pts) Answer: The real-axis crossing of the asymptote(s), a = The angle(s) of the asymptote(s), 0q = _ (b) Determine the break-away and the break-in points of the root-locus diagram for K > 0,...
Sketch the root locus for the unity feedback system shown in Figure P8.3 for the following...
Sketch the root locus for the unity feedback system shown in Figure P8.3 for the following transfer functions: (Section: 8.4] K(s + 2)(8 + 6) a. G(s) = 52 + 8 + 25 K( +4) b. G(S) = FIGURE PR3 152 +1) C G(s) - K(s+1) K (n1)(x + 4) For each system record all steps to sketching the root locus: 1) Identify the # of branches of the system 2) Make sure your sketch is symmetric about the real-axis...
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) contro...
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...
Q.10- For the system shown in Figure 5 with K (s + 3)(s +5) Gs)s-2)s-4) Find the range of gain, K, which will cause the system to be stable. Cs) Q.11. Draw the Root Locus of the following systems. Find the points of intersection with the real and imaginary axis. 6(s)H(s)- s(s +2) K(s+5) of- Draw the Bode diagram of the following tmamsfer finction. His)- -100 s +12s +21s +10 213- Obtain the phase and gain margins of the system...
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...
For the root locus shown below, find that makes s=-4 one of the closed loop system poles. Root Locus 15 10 Imaginary Axis (seconds) -10 -15 6 - 1 0 -3 -2 Real Axis (seconds)
Sketch the root locus for the control system shown in Figure Q3(b). b) Calculate the breakaway value of K and its location. Comment on the stability of the system. 1 G(s) and Ge(s) K (s+ 1) (s+2) where K is a positive constant C(s) R(s) G(s) Ge(s) Figure Q3(b) If the control system is modified by an addition of an open loop pole at s - 6 ii) 1 sketch the new root locus showing such that G(s) (s+1) (s+2)(s...
A system having an open loop transfer function of G(S) = K10/(S+2)(3+1) has a root locus plot as shown below. The location of the roots for a system gain of K= 0.248 is show on the plot. At this location the system has a damping factor of 0.708 and a settling time of 4/1.5 = 2.67 seconds. A lead compensator is to be used to improve the transient response. (Note that nothing is plotted on the graph except for that...
A plant with the transfer function Gp(s)-- with unity feedback has the root locus shown in the figure below: (s+2)(s+4) Root Locus 1.5 C(s) 0.5 0.5 1.5 .3 Real Axis (seconds) (a) Determine K of Gp(s) if it is desired that the uncompensated system has a 10% OS (overshoot) to a step input. (4 points) a 5% overshoot and a peak time Tp 3.1 meets the requirements described in part (b) and achieves zero steady state (b) Compute the desired...
Please solve part b and c and d !!
Consider the closed loop system shown in Figure 4. The root locus of that system is shown in Figure 5 (s+40s+8) R(s) Y(s) Figure 4 System block diagram of Problem 4 a) On the root locus plot, sketch the region of possible roots of the dominant closed-loop poles such that the system response to a unit step has the following time domain specifications. [5] i. Damping ratio, 20.76 ii. Natural frequency,....
9. Consider a negative unity-feedback control system with the loop transfer function s +8 D(s) G(8)=K- s+1) ((s + 1)2 + 22 (s + 94 + 793 + 1932 +33s + 20 (a) Determine the asymptotes of the root-locus diagram for K > 0, if any. (06pts) Answer: The real-axis crossing of the asymptote(s), a = The angle(s) of the asymptote(s), 0q = _ (b) Determine the break-away and the break-in points of the root-locus diagram for K > 0,...
Sketch the root locus for the unity feedback system shown in Figure P8.3 for the following transfer functions: (Section: 8.4] K(s + 2)(8 + 6) a. G(s) = 52 + 8 + 25 K( +4) b. G(S) = FIGURE PR3 152 +1) C G(s) - K(s+1) K (n1)(x + 4) For each system record all steps to sketching the root locus: 1) Identify the # of branches of the system 2) Make sure your sketch is symmetric about the real-axis...
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...
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