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control system
Problem 1) Consider the system shown in the figure. Plot the root loci. Locate...
Can you Solve in matlab please. I need your help B-7-6. Consider the system shown in Figure 7-59. Plot the root loci for the system. Determine the value of K such that the damping ratio ζ of the d...
Can you Solve in matlab please. I need your help
B-7-6. Consider the system shown in Figure 7-59. Plot the root loci for the system. Determine the value of K such that the damping ratio ζ of the dominant closed-loop poles is 05. Then determine all closed-loop poles. Plot the unit-step response curve with MATLAB. s(s2 +4s +5) Figure 7-59 Control system.
B-7-6. Consider the system shown in Figure 7-59. Plot the root loci for the system. Determine the value...
Please solve parts (a) and (b) neatly and show problem solving. Ignore reference to part 1, but please still plot the root loci. For the system given in Figure 1 a) Design a PD compensator with the t...
Please solve parts (a) and (b) neatly and show problem solving.
Ignore reference to part 1, but please still plot the root
loci.
For the system given in Figure 1 a) Design a PD compensator with the transfer function: to give a dominant root of the closed-loop characteristic equation of the compen- sated system at s -1+j1 (i.e., a settling time Ts of less than 6 seconds and a maximum overshoot Mo of less than 10%). Required Pre-Practical work] (b)...
(3) For the closed-loop system shown in the figure below, K varies from 0 to to. L(s) has 4 poles and no zero, and all the four poles are on the left half plane. Consider the root loci of L(s) fo...
(3) For the closed-loop system shown in the figure below, K varies from 0 to to. L(s) has 4 poles and no zero, and all the four poles are on the left half plane. Consider the root loci of L(s) for K approaching to too: how many branches of the root loci will be in the right half plane? (2 point) And Why? (2 points) L(s) Y(s) R(s) +
(3) For the closed-loop system shown in the figure below, K...
MECH 4310 Systems & Control Spring 2019 t) For the closed-loop system shown in the figure helow, K varies from 0 to to. Lo) has poles and no zero, and all the four poles are on the left hal...
MECH 4310 Systems & Control Spring 2019 t) For the closed-loop system shown in the figure helow, K varies from 0 to to. Lo) has poles and no zero, and all the four poles are on the left half plane. Consider the root loci of L(s) for K approaching to to: how many branches of the root loci will be in the right half plane? (2 point) And Why? (2 points) R(s)+ Y(s)
MECH 4310 Systems & Control Spring 2019...
Control System 3) Consider the simplified form of the transfer function for position servomechanism used in an antenna tracking system as shown in Figure Q3. By using root locus technique: Error Els)...
Control System
3) Consider the simplified form of the transfer function for position servomechanism used in an antenna tracking system as shown in Figure Q3. By using root locus technique: Error Els) C(s) R(s)+ s2 +4S +5 2.56S +12.8 Figure Q3 (a) Sketch its root locus (11 marks) (b) Find the value of K so that the damping ratio 0.342, and give all closed loop poles for the value of K. (9 marks)
3) Consider the simplified form of the...
3. Consider the system shown below. For this system. G(s) s(s+1)(s 2) H(s)1 We assume that the value of the gain K is nonnegative. Sketch the root locus plot and determine the K value such that the d...
3. Consider the system shown below. For this system. G(s) s(s+1)(s 2) H(s)1 We assume that the value of the gain K is nonnegative. Sketch the root locus plot and determine the K value such that the damping ratio of a pair of dominant complex-conjugate closed-loop poles is 0.5. Ri)1 C(s)
3. Consider the system shown below. For this system. G(s) s(s+1)(s 2) H(s)1 We assume that the value of the gain K is nonnegative. Sketch the root locus plot...
Consider the automobile cruise-control system shown below: Engine ActuatorCarburetor 0.833 and load 40 3s +1 Compensator R(s)E(s) Ge(s) s +1 -t e(t) Sensor 0.03 1) Derive the closed-loop transfer fun...
Consider the automobile cruise-control system shown below: Engine ActuatorCarburetor 0.833 and load 40 3s +1 Compensator R(s)E(s) Ge(s) s +1 -t e(t) Sensor 0.03 1) Derive the closed-loop transfer function of V(s)/R(s) when Gc(s)-1 2) Derive the closed-loop transfer function of E(s)/R(s) when Ge(s)-1 3) Plot the time history of the error e(t) of the closed-loop system when r(t) is a unit step input. 4) Plot the root-loci of the uncompensated system (when Gc(s)-1). Mark the closed-loop complex poles on...
Q.2. Using the multi-step procedure discussed in the class, plot the root loci for the unity-feedback...
Q.2. Using the multi-step procedure discussed in the class, plot the root loci for the unity-feedback system whose feed-forward transfer function is: s(s2+4s+5) Find the location of closed loop poles at K 2 (10 Points)
Due Date: April 20, 2 Problem 2: Consider a unity-feedback control system with the following open-loop...
Due Date: April 20, 2 Problem 2: Consider a unity-feedback control system with the following open-loop transfer function: K G(s)H(s) = s(s2 + 4s + 8) 1. Sketch the root-locus plot. 2. IfK 2, where are the closed-loop poles located? 3. If x = 0.5, where are the closed-loop poles located?
54 + 1.15 + 10.35 + 5s Plot the root loci for the system with MATLAB...
54 + 1.15 + 10.35 + 5s Plot the root loci for the system with MATLAB "roblem B-10-17 Plorthe root face for the system shown in Figure 10-10-Determine the range of gain K required for stability. Using Routh's stability criterion s(s+2) -105 Control system obleme 10 10
Can you Solve in matlab please. I need your help
B-7-6. Consider the system shown in Figure 7-59. Plot the root loci for the system. Determine the value of K such that the damping ratio ζ of the dominant closed-loop poles is 05. Then determine all closed-loop poles. Plot the unit-step response curve with MATLAB. s(s2 +4s +5) Figure 7-59 Control system.
B-7-6. Consider the system shown in Figure 7-59. Plot the root loci for the system. Determine the value...
Please solve parts (a) and (b) neatly and show problem solving.
Ignore reference to part 1, but please still plot the root
loci.
For the system given in Figure 1 a) Design a PD compensator with the transfer function: to give a dominant root of the closed-loop characteristic equation of the compen- sated system at s -1+j1 (i.e., a settling time Ts of less than 6 seconds and a maximum overshoot Mo of less than 10%). Required Pre-Practical work] (b)...
(3) For the closed-loop system shown in the figure below, K varies from 0 to to. L(s) has 4 poles and no zero, and all the four poles are on the left half plane. Consider the root loci of L(s) for K approaching to too: how many branches of the root loci will be in the right half plane? (2 point) And Why? (2 points) L(s) Y(s) R(s) +
(3) For the closed-loop system shown in the figure below, K...
MECH 4310 Systems & Control Spring 2019 t) For the closed-loop system shown in the figure helow, K varies from 0 to to. Lo) has poles and no zero, and all the four poles are on the left half plane. Consider the root loci of L(s) for K approaching to to: how many branches of the root loci will be in the right half plane? (2 point) And Why? (2 points) R(s)+ Y(s)
MECH 4310 Systems & Control Spring 2019...
Control System
3) Consider the simplified form of the transfer function for position servomechanism used in an antenna tracking system as shown in Figure Q3. By using root locus technique: Error Els) C(s) R(s)+ s2 +4S +5 2.56S +12.8 Figure Q3 (a) Sketch its root locus (11 marks) (b) Find the value of K so that the damping ratio 0.342, and give all closed loop poles for the value of K. (9 marks)
3) Consider the simplified form of the...
3. Consider the system shown below. For this system. G(s) s(s+1)(s 2) H(s)1 We assume that the value of the gain K is nonnegative. Sketch the root locus plot and determine the K value such that the damping ratio of a pair of dominant complex-conjugate closed-loop poles is 0.5. Ri)1 C(s)
3. Consider the system shown below. For this system. G(s) s(s+1)(s 2) H(s)1 We assume that the value of the gain K is nonnegative. Sketch the root locus plot...
Consider the automobile cruise-control system shown below: Engine ActuatorCarburetor 0.833 and load 40 3s +1 Compensator R(s)E(s) Ge(s) s +1 -t e(t) Sensor 0.03 1) Derive the closed-loop transfer function of V(s)/R(s) when Gc(s)-1 2) Derive the closed-loop transfer function of E(s)/R(s) when Ge(s)-1 3) Plot the time history of the error e(t) of the closed-loop system when r(t) is a unit step input. 4) Plot the root-loci of the uncompensated system (when Gc(s)-1). Mark the closed-loop complex poles on...
Q.2. Using the multi-step procedure discussed in the class, plot the root loci for the unity-feedback system whose feed-forward transfer function is: s(s2+4s+5) Find the location of closed loop poles at K 2 (10 Points)
Due Date: April 20, 2 Problem 2: Consider a unity-feedback control system with the following open-loop transfer function: K G(s)H(s) = s(s2 + 4s + 8) 1. Sketch the root-locus plot. 2. IfK 2, where are the closed-loop poles located? 3. If x = 0.5, where are the closed-loop poles located?
54 + 1.15 + 10.35 + 5s Plot the root loci for the system with MATLAB "roblem B-10-17 Plorthe root face for the system shown in Figure 10-10-Determine the range of gain K required for stability. Using Routh's stability criterion s(s+2) -105 Control system obleme 10 10
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