The objective of the controller design in Fig. 1 is to find the controller Gc(s) such that I.)The closed-loop system is stable ii.)The output of the system above (y(t)) can track the reference input r(t) = At (A>0 is any real number). Use the Nyquist plot and Nyquist criterion to show that: a.)The portional controller Gc(s)=K can achieve asymptotic tracking of the ramp input r(t)=At but cannot meet the stability requirement for 0<K<+inf. b.) Can the PI controller Gc(s)=K(1+10/s) be used to meet the requirements I.) - ii.)? Please use the Nyquist plot and Nyquist criterion, together with the steady-state analysis, to prove your conclusion. c.) Can the PI controller Gc(s)=K(1+10/s) be used to track the input signal r(t)=At^2 for any A>0? Prove or disprove your answer.
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SUMMARY: here we have to find out characteristic equation of closed loop trnsfer function and cheack for stability before continuing furthur analysis we must ensure weather the system is stable or not.We have to apply laplase trasform to convert time domain input into s domain.
trick:while drawing nyquist plot you can follow these three simple steps
i)draw polar plot
ii)draw its mirror image
iii)join the mirror image end direction with polar plot starting direction
HOPE THIS HELPS YOU!!
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The objective of the controller design in Fig. 1 is to find the controller Gc(s) such...
Q.3(a) Transfer function model of a plant is, G(s) The controller is Ge(s)-K, where K is a constant. Find the value of K such that steady-state error for unit ramp input is 0.1. Find the gain margin and the phase mar gin (6 marks) (b) What are the effects on gain margin, phase margin and steady-state error, if the gain K is increased? (3 marks (c) Can the closed loop be unstable if the controller of Q.3(a) is implemented digi...
1. A feedback control system is shown in the figure below. Suppose that our design objective is to find a controller Gc(S) of minimal complexity such that our closed-loop system can track a unit step input with a steady-state error of zero. (b) Now consider a more complex controller Gc(S) = [ Ko + K//s] where Ko = 2 and Ki = 20. (This is a proportional + integral (PI) controller). Plot the unit step response, and determine the steady-state...
6 and controller C(s), as shown in the Consider a unity-feedback control system with plant G(s)- following figure. Reference Error Controller Plant r(t) e(t) u(t) y(t) C(s) G(s) [5] (a) Determine the poles, zeros, order, type, relative degree, and de gain of the plant G(s) and show [5] (b) Can a P controller C(s)Kp stabilize the plant G(s)? If so, find the values of Kp that are [4] (c) Show using the Final Value Theorem that the system with the...
Sketch the Nyquist plots of the following loop transfer functions L(S) = Gc(s)G(s), and determine whether the system is stable by applying the Nyquist criterion: KS + 1) (b) L(s) = G (9)G(s) = 318+) If the system is stable, find the maximum value for K by determining the point where the Nyquist plot crosses the u-axis.
3. Design a PI or PD controller for the system G(8) = s(s+10) to meet the following specifications • Zero steady state error for unit step reference input • tr< 0.12 - . %OS < 10%. (a) Determine the low frequency gain, crossover frequency and phase margin necessary to meet the specifications. (b) Decide if C(s) needs an integrator. Plot the Bode plot of either G(s) or G(s)/s, depending on your choice. (c) Use sisotool (or iteration) to choose a...
PLEASE, the problem states that Gc(s)=K/(s+90), not just K. The design has the controller with a real pole. S=-90. In a standard unity-feedback system, lt the transfer finction of the plant be G(G) 1)(a5) → c(s) Design Objectives 1) The closed-loop system is stable 2) The percent overshoot of the unit-step response ofc(t) does not exceed 15% 3) The steady-state error due to a unit-step reference input is as small as possible.
G) r(t) Figure 1: Feedback control system A pulley and belt transmission has a linearized relationship between the driven pulley angle θ(t) in degrees and the input torque u(t) in Newton meters given by the following differential equation du(t) A feedback control system (illustrated in Figure 1) needs to be designed such that the closed-loop system is asymptotically stable and such that the following design criteria are met: 1. the gain crossover frequency a should be between and a 2....
1472) The plant of a magnetic-gap controller is: Gp(s)=1/((s+f)(s-f)). A controller Gc(s)=K(s+b)(s+c)/s is proposed. Determine the gain K for marginal stability. b=0.70, c=104.00, f=62.90. Determine the gain K for CLGM = 10 dB. Gp & Gs are in the forward path of unity feedback sys. ans:2
(2.) Consider the simplified satellite altitude control problem shown below. Design an appropriate controller to meet the following specifications (10 Marks) (a) The percent overshoot for a step input is s 5% The settling time (with a 2 % criterion) is T 6 sec The system velocity (b) (c) error constant K.> 1 R(s) E(s) Y(s) Controller (s1)(s5) Plant (2.) Consider the simplified satellite altitude control problem shown below. Design an appropriate controller to meet the following specifications (10 Marks)...
1472) The plant of a magnetic-gap controller is: Gp(s)=1/((s+f) (S-f)). A controller Gc(s)=K (s+b) (s+c)/s is proposed. Determine the gain K for marginal stability. b=0.20, c=103.00, f=66.50. Determine the gain K for CLGM=10.9 dB. Gp & Gs are in the forward path of unity feedback sys. ans:2 Illat