Given a Bode diagram of a dynamic system, shown in Fig. 4: (a) Find the transfer function of the system G(s) (asymptotes are drawn for you and their slopes are indicated) T (b) Derive the open-loop system response to a harmonic input 2 cos 10t+- (c) Assuming a negative unity feedback configuration: Determine the gain and phase margins of the system Is the system closed-loop stable? Verify your answer using Nyquist plot (use software to generate Nyquist plot and explain how it confirms your conclusion of closed-loop stability/instability) (d) Assuming a proportional controller with gain Kp and negative unity feedback configuration: Can the system be destabilized by a finite gain proportional controller? If yes, find the gain K, that destabilizes the system. If not, explain why not. (e) Find Kp for the system to have a phase margin 20⁰ (f) What is the system phase margin when Kp = 10? At this value of Kp: What is the steady-state error of the closed-loop system to a step input of magnitude A? ● ● ● What is the steady-state error of the closed-loop system to a ramp input of magnitude A? NOTE: parts (b), (c), (e), (f) need to be solved graphically

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Given a Bode diagram of a dynamic system, shown in Fig. 4:
(a) Find the transfer function of the system G(s)
(asymptotes are drawn for you and their slopes are indicated)
(b) Derive the open-loop system response to a harmonic input 2 cos 10t+ 44
(c) Assuming a negative unity feedback configuration:
Determine the gain and phase margins of the system
Is the system closed-loop stable? Verify your answer using Nyquist plot (use software
to generate Nyquist plot and explain how it confirms your conclusion of closed-loop
stability/instability)
(d) Assuming a proportional controller with gain K₂ and negative unity feedback
configuration:
Can the system be destabilized by a finite gain proportional controller? If yes, find the
gain Kp that destabilizes the system. If not, explain why not.
(e) Find Kp for the system to have a phase margin 20⁰
(f) What is the system phase margin when K₂ = 10? At this value of Kp:
What is the steady-state error of the closed-loop system to a step input of magnitude
A?
|G(jw)|, dB
●
ø, degrees
●
NOTE:
parts (b), (c), (e), (f) need to be solved graphically
What is the steady-state error of the closed-loop system to a ramp input of magnitude
A?
0
-20
-40
-60
-80
0.01
50
0
-50
-100
-150
0.01
20 dB dec
0.1
0.1
1
1
0 dB/dec
w, rad/sec
w, rad/sec
Figure 4
10
10
↑hump
40 dB/dec
100
100
1000
1000
Transcribed Image Text:Given a Bode diagram of a dynamic system, shown in Fig. 4: (a) Find the transfer function of the system G(s) (asymptotes are drawn for you and their slopes are indicated) (b) Derive the open-loop system response to a harmonic input 2 cos 10t+ 44 (c) Assuming a negative unity feedback configuration: Determine the gain and phase margins of the system Is the system closed-loop stable? Verify your answer using Nyquist plot (use software to generate Nyquist plot and explain how it confirms your conclusion of closed-loop stability/instability) (d) Assuming a proportional controller with gain K₂ and negative unity feedback configuration: Can the system be destabilized by a finite gain proportional controller? If yes, find the gain Kp that destabilizes the system. If not, explain why not. (e) Find Kp for the system to have a phase margin 20⁰ (f) What is the system phase margin when K₂ = 10? At this value of Kp: What is the steady-state error of the closed-loop system to a step input of magnitude A? |G(jw)|, dB ● ø, degrees ● NOTE: parts (b), (c), (e), (f) need to be solved graphically What is the steady-state error of the closed-loop system to a ramp input of magnitude A? 0 -20 -40 -60 -80 0.01 50 0 -50 -100 -150 0.01 20 dB dec 0.1 0.1 1 1 0 dB/dec w, rad/sec w, rad/sec Figure 4 10 10 ↑hump 40 dB/dec 100 100 1000 1000
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