8. (10 pts.) Design a stabilizing, first-order compensator to place the dominant closed- loop poles at zs-0.5 +j0.5 for G[z]- 8. (10 pts.) Design a stabilizing, first-order compensator to place...
2. Controller Design For each of the following plants G, design a compensator G, so that the closed loop system KG, G (1 + KG, G has two dominant poles near 2 ± i Plot a root locus plot for the system before adding the compensator and another plot for after. Use the simplest G that you can find. Determine the gain K that will achieve the desired poles 142 2. Controller Design For each of the following plants G,...
Problem 2: Given the plant G,le)+2( +3) design a PI compensator Gc(s)-K Ш such the closed-loop unity feedback system has two dominant poles at s1.2 =-1 ±j. Using Matlab ritool (or simulink), simulate your closed loop system to show that the unit-step response of the system has PO ~ 4.3%, tr 2.35 sec, and 4 ะ 4.15 sec. Compute the closed-loop poles and zeros.
4. A lead compensator with a transfer function Ge(s)=K(+0.5/(s+3) has been designed for a Space vehicle with the transfer function 1/s' such that at the dominant closed loop poles are located at -1 +/-j1. (0) What is the angle deficiency of the uncompensated system at the designed point provided by the location of the dominant poles? Show that the compensator provides the necessary lead angle at the designed point to satisfy the root locus angle criterion. What value of K...
the place poles are -2 ; -3 ; -4 Design a state feedback control u=-Kx, Find K, that could place the closed loop poles at-21 -3,-4 Given that: Consider the systemi Ar Bu with A-10-201. B-10 1 2) Exploiting the structure of A and B, find a different feedback gain that place the poles in the same location. This steps shows that there are several ways to design K; by inspection for instance. Design a state feedback control u=-Kx, Find...
7. Consider the following closed-loop system in which G(s5 Design a lag compensator, Ge( steady-state error due to a ramp input is 2% of the velocity of the ramp and the phase margin is 45°. 7. Consider the following closed-loop system in which G(s5 Design a lag compensator, Ge( steady-state error due to a ramp input is 2% of the velocity of the ramp and the phase margin is 45°.
Design of PID compensator S. Design of PID (Proportional-plus-Integral and Derivative) Compensator ds/i (st3)(s+6 s+10) and unity feedback Design a PID s+10) An uncompensated system has a gain controller so that the system can operate with a peak time that is two thirds that of the uncompensated system at 20% overshoot and with zero steady-state error for a step input. system has a gain Uncompensated system Compensated system K (s+8 G(s) = (s+3)(s+6)(s+10) ,H(s) = 1 20% OS; desired T,-23a...
For the given system, find the full-state feedback gain matrix, K, to place the closed-loop poles at z - 0.9 1j0.1. 1. x(n + 1)-φχ(n) + l'u(n), with 0.5
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...
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)...
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: •...