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Please answer this question showing all the steps. Problem 1 Suppose we have the system shown below operating at 1 0% overshoot. Go) +s+2)(+1 52 05123 120 Design changing the dominant pole locati...
Problem 4 Suppose we have the system shown below operating at 15% overshoot. G(s)- (G) (s +2)%s +5%s+7) Use time domain techniques to design a compensator (and find K) so the appropriate static e...
Problem 4 Suppose we have the system shown below operating at 15% overshoot. G(s)- (G) (s +2)%s +5%s+7) Use time domain techniques to design a compensator (and find K) so the appropriate static error constant is 20 without appreciably changing the dominant poles of the uncompensated system. There can be no zero pole cancellations. Do not change the dominant poles of the system.
Problem 4 Suppose we have the system shown below operating at 15% overshoot. G(s)- (G) (s +2)%s...
Problem (5): . The unity feedback system shown in Figure P9.1 with is operating with 10% overshoo...
Problem (5): . The unity feedback system shown in Figure P9.1 with is operating with 10% overshoot [Section: 9 21 R. Whai is the value of the appropriate static error constant? b. Find the transfer function of a lag network so that the appropriale static error constant equals 4 without appreciably changing he dominant poles of the uncompensated system e. Use MATLAB or any other computer MATLAD progtam to si mulatcthe system o seethe effect of your compensator ML C(F)...
For the control system shown below G(8) (8+10) 6+20) U(8) Y(8) H(s) = 1 design (using...
For the control system shown below G(8) (8+10) 6+20) U(8) Y(8) H(s) = 1 design (using the Root-Locus Method) a compensator so that: • static velocity error constant K = 41 • the dumping ratio Efor dominant poles will remain unchanged, • a small change of undamped natural frequency oon is acceptable. sec For the control system shown below + G(S) = 820 s(8+10)(8+20) U(s) Y(s) H(s) = 1 design (using the Root-Locus Method) a LAG-LEAD compensator so that: •...
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...
Problem 4. Consider the control system shown below with plant G(s) that has time con- stants...
Problem 4. Consider the control system shown below with plant G(s) that has time con- stants T1 = 2, T2 = 10, and gain k = 0.1. 4 673 +1679+1) (1.) Sketch the pole-zero plot for G(s). Is one of the poles more dominant? Using MATLAB, simulate the step response of the plant itself, along with G1(s) and G2(s) as defined by Gl(s) = and G2(s) = sti + 1 ST2+1 (2.) Design a proportional gain C(s) = K so...
Problem 4 Suppose we have the system shown below operating at 15% overshoot. G(s)- (G) (s +2)%s +5%s+7) Use time domain techniques to design a compensator (and find K) so the appropriate static error constant is 20 without appreciably changing the dominant poles of the uncompensated system. There can be no zero pole cancellations. Do not change the dominant poles of the system.
Problem 4 Suppose we have the system shown below operating at 15% overshoot. G(s)- (G) (s +2)%s...
Problem (5): . The unity feedback system shown in Figure P9.1 with is operating with 10% overshoot [Section: 9 21 R. Whai is the value of the appropriate static error constant? b. Find the transfer function of a lag network so that the appropriale static error constant equals 4 without appreciably changing he dominant poles of the uncompensated system e. Use MATLAB or any other computer MATLAD progtam to si mulatcthe system o seethe effect of your compensator ML C(F)...
For the control system shown below G(8) (8+10) 6+20) U(8) Y(8) H(s) = 1 design (using the Root-Locus Method) a compensator so that: • static velocity error constant K = 41 • the dumping ratio Efor dominant poles will remain unchanged, • a small change of undamped natural frequency oon is acceptable. sec For the control system shown below + G(S) = 820 s(8+10)(8+20) U(s) Y(s) H(s) = 1 design (using the Root-Locus Method) a LAG-LEAD compensator so that: •...
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...
Problem 4. Consider the control system shown below with plant G(s) that has time con- stants T1 = 2, T2 = 10, and gain k = 0.1. 4 673 +1679+1) (1.) Sketch the pole-zero plot for G(s). Is one of the poles more dominant? Using MATLAB, simulate the step response of the plant itself, along with G1(s) and G2(s) as defined by Gl(s) = and G2(s) = sti + 1 ST2+1 (2.) Design a proportional gain C(s) = K so...
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