please solve as matlab code. The system in Figure 3 comprises a motor and a contoller. The performance requirements entail a steady state error for ramp input r(t) Ct, smaller than 0.01C. Here, C...
Write as MATLAB code with comments thank you. The system in Figure 3 comprises a motor and a contoller. The performance requirements entail a steady state error for ramp input r(t) Ct, smaller than 0.01C. Here, C is a constant. The overshoot for step input must be such that P.0.S 5% and the settling time with a 2% error should be T. 2 seconds. (a) Based on rlocus function, write a piece of MATLAB code which establishes the controller. (b)...
PLEASE SOLVE IN MATLAB !!!!!! PLEASE SOLVE IN MATLAB !!!!!! PLEASE SOLVE IN MATLAB !!!!!! PLEASE SOLVE IN MATLAB !!!!!! PLEASE SOLVE IN MATLAB !!!!!! PLEASE SOLVE IN MATLAB !!!!!! PLEASE SOLVE IN MATLAB !!!!!! PLEASE SOLVE IN MATLAB !!!!!! PLEASE SOLVE IN MATLAB !!!!!! PROBLEM 3 The system in Figure 3 comprises a motor and a contoller. The performance requirements entail a steady state error for ramp input r(t)-Ct, smaller than 0.01C. Here, C is a constant. The overshoot...
Please show calculations by HAND and NOT MATLAB. The answers are here to help. Thank you Note : Ts= 4/&*wn (&=damping ratio) Skill-Assessment Exercise 9.3 PROBLEM: A unity feedback system with forward transfer function 6) s(s + is operating with a closed-loop step response that has 20% overshoot. Do the following: a. Evaluate the settling time. b. Evaluate the steady-state error for a unit ramp input. c. Design a lag-lead compensator to decrease the settling time by 2 times and...
Consider the closed loop systema) Design a PD controller (that is, calculate K1 and K2) such that the system isstable and the steady-state error for the input r (t) = unity ramp letless than or equal to 0.02.b) Select a value from K1 and K2 and build the model in Simulink or solutionanalytical to obtain the response of the system to the magnitude rampr (t) = 2t.c) Graph the answer
PLEASE USE MATLAB TO ANSWER ALL OF THE PARTS. PROVIDE MATLAB CODE FOR EACH OF THE PART. PUT THE ANSWER IN A BOX. Consider the unity feedback system depicted in Figure 1 G(s) R(s) 50K s(s + a) Figure 1 1. Determine the system's closed loop transfer function. 2. Plot the system's step response for K=10 and: • a= 2 • a=5 • a= 10 3. What happens to the system's response as a increases? Justify your answer. 4. In...
Question 2 Consider the system shown in Figure Q2, where Wis a unit step disturbance and R is a unit step input. 0.4 s+ 1 10 Figure Q2 (5 marks) (3 marks) (c) Find the value for K so that the steady state error due to w(t) is less than 0.01; 6 marks) (d) In order to eliminate the steady state error, show whether a PI controller can be successful 6 marks) (a) Find the expression of E(s)-R(s)-Y(s) in terms...
Question 2 Consider the system shown in Figure Q2, where Wis a unit step disturbance and R is a unit step input. 0.4 s+ 1 10 Figure Q2 (5 marks) (3 marks) (c) Find the value for K so that the steady state error due to w(t) is less than 0.01; 6 marks) (d) In order to eliminate the steady state error, show whether a PI controller can be successful 6 marks) (a) Find the expression of E(s)-R(s)-Y(s) in terms...
PLEASE solve it with 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 Isim function of MATLAB, calculate and obtain the graph of the response for 6, (t)-at. Here a : 0.5%, Find the height error after 10 seconds, G) -2 This is a Proportional-Integral (PI) controller. Repeat part (a) in the presence of Pl controller, and juxtapose the steady state error...
Please answer all the questions with MATLAB and also upload the code. Thanks. 3 Experiment - Matlab controller complexity and steady-state 3.1 Consider the satellite-attitude control problem shown in following figure where the normalized parameters are J 10 spacecraft inertia; N-m-sec2 /rad erreference satellite attitude; rad actual satellite attitude; rad Hy 1 sensor scale; factor volts/rad Hr = 1 reference sensor scale factor ; volts/rad w= disturbance torque: N-m H, D(s) Js Figure 4: Satellite attitude control Suppose kP =...
R(S) C(s) G(s) Figure P3 G(S) K(s2 – 2s + 2) s(s + 1)(8 +2) Problem 4) (25 points) Consider the same unity feedback control system given in Figure P3 and do the following: a. Determine the system type (type 0, type 1, type 2, etc.) and justify it. (05 points) b. Suppose that 10% maximum overshoot is required as a transient response specification. Find the steady-state error for this P-controlled system, where K = 0.24 for a unit step...