06)= 7+3+ 3 +2" (+3&+2+1) TO 53 +352 + 3s + 2 (5+2) (++1) R(S 25....
2 Find the inverse Laplace transforms of 5 7 R(s) 3-+ 3s+7 Qs)(s+2)2+25 a. b.
PLEASE SOLVE IT ASAP ! WITH CLEAR STEPS !!
2. (30 points) For the closed-loop control system shown below, C(s) R(s) 0.5 3s +1 1) Please find the closed-loop transfer function C(s)/R(s). (15 points) 2) Without mathematically solving the response c(), please plot c() to a unit step input (r(t)-1). (15 points)
2. (30 points) For the closed-loop control system shown below, C(s) R(s) 0.5 3s +1 1) Please find the closed-loop transfer function C(s)/R(s). (15 points) 2) Without mathematically...
could you please answer this question
QUESTION 2 Consider a system with an open-loop trans fer function given by Y(s) s+7 U(s) s2 +3s-8 (a) (8 marks) Derive a state-space model for the system in canonical form. (b) (4 marks) Check the observability of the system. (c) 8 marks) Design a suitable full-order state observer for the system. Explain your choice of the observer's poles. d) (10 marks) Design a PI controller for the system so the output of the...
Given the following system, where Gs(s) - -e2) Given the following system, where Gc(s) S+3 3s++2) and H(s)s R(S) . Gc(s) G(s) Y(s) SOLVE IN MATLAB CODE ONLY Obtain the transfer function of the system above. Find zeros, poles, and gain of the transfer function and plot zeros and poles. Rewrite the transfer function using the partial fraction expansion. Graph the Step response. Graph the impulse response.
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...
(10 points each) Given the following unity feedback system 3. E(s) R(s) C(s) 080-00 Figure 3 Where Go) DXG+3%6+5) 2(s +2) Find stability, and how many poles are in the right half-plane, in the left half-plane, on the jw axis. a. b. Draw the root locus for the system indicating the breakaway points, the ju crossings Draw the corresponding asymptotes on the diagram, calculate number of asymptotes, center and angle of asymptotes. c.
(10 points each) Given the following unity...
Consider the unity feedback system shown below R(s) C(s) Gp(s) 5(s+6 with G,(6)(s +2)(s+25) You are given that s+27s +55s+30 is a stable polynomial. a. What is the system type? For the questions below (in this Problem), set K-1 b. Determine the error constants Ko, K, and K, (also known as K,K, and K, c. Determine the steady-state errors eo, ei, and e2 (also known as epey, and e.) d. What is the steady-state error if the input is 5tu(t)?
Question 2. The transfer Function of a feedback control loop is given by: C(s)- R(s) (3s + where Ke is the controller gain. Derive the relationships between the gain, time constant, and damping ratio of the second-order transfer function to the controller gain. Find the ranges of the controller gain for which the response is (i) overdamped, (ii) underdamped, and (iii) undamped. Can the response be unstable for any positive values of the controller gain? x (s) y(s) = {1...
Consider the following control system: R + Let G(s) s +23-3 and H(s) K where K is some positive constant. The transfer function H(s) can be considered a proportional feedback controller. (a) Examine the behavior of the system for different values of K. Try the values K 2, 4, 8. In each case, plot the pole-zero map of the closed-loop system and examine the step response. Comment on the stability of the system. Find the value of K for which...
1- [a] For positive values of K, plot the root locus for a unity negative feedback control system having the following open-loop transfer function: K G(s)= (5 + 1)(8 + 4)(8 + 7) For what values of gain K does the system become unstable? Find also the value of k at which the damping ratio is 0.5 and the closed loop poles. (25%) [b] The characteristic equations of linear control systems are given below. Apply Routh-Hurwitz criterion to determine the...