Output Lamput Rato controller - Part Y(s) U(s) ms + b Using proportional control. Y(s) ko...
PLEASE DO IN MATLAB
Problem 8 (PID feedback control). This problem is about Proportional-Integral-Derivative feedback control systems. The general setup of the system we are going to look at is given below: e(t) u(t) |C(s) y(t) P(s) r(t) Here the various signals are: signal/system r(t) y(t) e(t) P(s) C(s) и(t) meaning desired output signal actual output signal error signal r(t) y(t) Laplace transform of the (unstable) plant controller to be designed control signal Our goal is to design a controller...
PROBLEMA: (25%) A closed-loop control system is shown below Ds) T(O) U(A) C(s) (a) Show that a proportional controller (C(s)-kp) will never make the closed-loop system stable. (8%) (Hint: you need to calculate the closed-loop pole locations and make discussion for the two possible cases.) (Medim) (b) When a PD controller is used (C(s)kp+ kps), calculate the steady state tracking error when both R(s) and D(s) are unit steps. (8%) (Easy) (e) Suppose R(s) is a unit step and D(s)...
Consider the following closed-loop system, where Y(s) R(s)+ KcP Ks Assume the following nominal values: Ko-2. 〈 = 0.8; ω,-4; Ks-2. Use transfer function sensitivity calculations in answering the questions below. a) With proportional controller gain K 10 and r(t) a step input, determine the percentage change in steady-state output y(t) if Ko increases 5% from its nominal value. (12 pts.) b) Repeat part (a) with Kc - 50. (6 pts.) c) With proportional controller gain Kc 10 and r(t)...
Question 4 (a) A feedback control system with a proportional controller is shown in Figure Q4 (a). (i) Sketch the root locus of the system, (ii) Design the proportional controller (choose the value of K) such that the damping ratio does not exceed 0.5 and the time constant is less than 1 second. [All necessary steps of root locus construction and controller design must be shown). C(s) R(S) + s(s+4)(s + 10) Figure Q4 (a). A feedback control system [11...
Question 6 The open-loop transfer function G(s) of a control system is given as G(8)- s(s+2)(s +5) A proportional controller is used to control the system as shown in Figure 6 below: Y(s) R(s) + G(s) Figure 6: A control system with a proportional controller a) Assume Hp(s) is a proportional controller with the transfer function H,(s) kp. Determine, using the Routh-Hurwitz Stability Criterion, the value of kp for which the closed-loop system in Figure 6 is marginally stable. (6...
Using MATLAB. We want to control output(y) using PID control in Kds? +Kps+Ki C(s) S Input(r) is a magnitude1 step. Plant is given by 1 (s+1)(s+2)(s+59) controller plant 14 y C(s) P(S) a) Calculate Closed Loop characteristics and steady-state error(unity feedback and Kp=1, Kd=1, Ki=0)) 2.Using automatic PID tuning function, reduce steady-state error=0 and report Kp=?, Kd=? And Ki=?
Using MATLAB. We want to control output(y) using PID control in Kds? +Kps+Ki C(s) S Input(r) is a magnitude1 step. Plant is given by 1 (s+1)(3+2)(s+5 ) controller plant + 14 y C(s) P(S) a) Calculate Closed Loop characteristics and steady-state error(unity feedback and Kp=1, Kd=1, Ki=0)) 2.Using automatic PID tuning function, reduce steady-state error=0 and report Kp=?, Kd=? And Ki=?
2nd. In the control system below; w(s) + R(s) E(s) Y(s) Ko+Kp.s s(s+1) Sistem a. The damping factor is & = 0.5 and the complex conjugate poles of the closed loop system K for real part to be -2p and Ko Calculate the values that should be taken. ( 10p) b. Find the absolute value of the continuous regime error against the unit step-breaking effect. This error how to minimize. (20p) c. K to PD, When s is added; K...
We want to control output(y) using PID control in Kds2+KpS+Ki C(s) S Input(r) is a magnitude1 step. Plant is given by 1 (s+1)(s+2)(s+5) controller plant Y C(s) P(s) a) Calculate Closed Loop characteristics and steady-state error(unity feedback and Kp=1, Kd=1, Ki=0)) 2.Using automatic PID tuning function, reduce steady-state error=0 and report Kp=?, Kd=? And Ki=?
This feedback control system represents Integral Control of a Mass-Spring-Damper system: Controller Mass-Spring-Damper R(S) + Y(s) 17 S2 + 2s +6 NOTE: 1) Integral control is being used here (i.e. C(s) = Determine the values of gain "K,” for which the closed-loop system (i.e. RS ) remains stable.