Calculate the damping ratio and natural frequency of the closed-loop system for K=10 and K=25.
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Calculate the damping ratio and natural frequency of the
closed-loop system for K=10 and K=25....
25 points Save The figure shows a closed-loop system What is the kp value to keep...
25 points Save The figure shows a closed-loop system What is the kp value to keep the system with a damping ration= 7/10? Plant disturbance Reference command + Control input System output error Kp 21(s+1) Feedback 6/(S+6)
Problem 4 (25%) Consider the attitude control system of a rigid satellite shown in Figure 1.1....
Problem 4 (25%) Consider the attitude control system of a rigid satellite shown in Figure 1.1. Fig. 1.1 Satellite tracking control system In this problem we will only consider the control of the angle e (angle of elevation). The dynamic model of the rigid satellite, rotating about an axis perpendicular to the page, can be approximately written as: JÖ = tm - ty - bė where ) is the satellite's moment of inertia, b is the damping coefficient, tm is...
Problem 3 (25 points): Consider the following closed-loop control system K(s +9) (s4s + 11) A....
Problem 3 (25 points): Consider the following closed-loop control system K(s +9) (s4s + 11) A. Plot the open-loop poles and zeros on a graph. B. Compute and draw an C. Compute any break-away and break-in points. D. Compute any jo crossings. E. Draw a qualitatively-correct root locus diagram. y asymptote real intercepts and angles. Locate the closed-loop poles on the root locus plot such that the don closed-loop poles have a-damping-ratio equal to.0.5,and-determine corresponding value of the gainK.-
The parameters are as follows k=10 a=0.50 b=0.3 c=0.6 d=9 w_1=12 w_2=15 Kv=30 A feedback control system (illustrated in Figure 1) needs to be designed such that the closed-loop system is asymptotical...
The parameters are as follows
k=10 a=0.50 b=0.3 c=0.6 d=9 w_1=12 w_2=15
Kv=30
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:
the gain crossover frequency wc should be between
w1 and w2.
the steady-state error should be zero in response to a unit
step reference.
the velocity constant should be greater than Kv (in
other words, the steady-state unit...
The parameters are as follows k=10 a=0.50 b=0.3 c=0.6 d=9 w_1=12 w_2=15 Kv=30 A feedback control system (illustrated in Figure 1) needs to be designed such that the closed-loop system is asymptotical...
The parameters are as follows
k=10 a=0.50 b=0.3 c=0.6 d=9 w_1=12 w_2=15
Kv=30
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:
the gain crossover frequency wc should be between
w1 and w2.
the steady-state error should be zero in response to a unit
step reference.
the velocity constant should be greater than Kv (in
other words, the steady-state unit...
25 points Save The figure shows a closed-loop system What is the kp value to keep the system with a damping ration= 7/10? Plant disturbance Reference command + Control input System output error Kp 21(s+1) Feedback 6/(S+6)
Problem 4 (25%) Consider the attitude control system of a rigid satellite shown in Figure 1.1. Fig. 1.1 Satellite tracking control system In this problem we will only consider the control of the angle e (angle of elevation). The dynamic model of the rigid satellite, rotating about an axis perpendicular to the page, can be approximately written as: JÖ = tm - ty - bė where ) is the satellite's moment of inertia, b is the damping coefficient, tm is...
Problem 3 (25 points): Consider the following closed-loop control system K(s +9) (s4s + 11) A. Plot the open-loop poles and zeros on a graph. B. Compute and draw an C. Compute any break-away and break-in points. D. Compute any jo crossings. E. Draw a qualitatively-correct root locus diagram. y asymptote real intercepts and angles. Locate the closed-loop poles on the root locus plot such that the don closed-loop poles have a-damping-ratio equal to.0.5,and-determine corresponding value of the gainK.-
The parameters are as follows
k=10 a=0.50 b=0.3 c=0.6 d=9 w_1=12 w_2=15
Kv=30
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:
the gain crossover frequency wc should be between
w1 and w2.
the steady-state error should be zero in response to a unit
step reference.
the velocity constant should be greater than Kv (in
other words, the steady-state unit...
The parameters are as follows
k=10 a=0.50 b=0.3 c=0.6 d=9 w_1=12 w_2=15
Kv=30
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:
the gain crossover frequency wc should be between
w1 and w2.
the steady-state error should be zero in response to a unit
step reference.
the velocity constant should be greater than Kv (in
other words, the steady-state unit...
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