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6. Consider a state-space system x = Ax+ Bu, y = Cx for which the control...
3. Consider a system with the following state equation h(t)] [0 0 21 [X1(t) [x1(t) y(t)...
3. Consider a system with the following state equation h(t)] [0 0 21 [X1(t) [x1(t) y(t) [0.1 0 0.1x2(t) X3(t) The unit step response is required to have a settling time of less than 2 seconds and a percent overshoot of less than 5%. In addition a zero steady-state error is needed. The goal is to design the state feedback control law in the form of u(t) Kx(t) + Gr(t) (a) Find the desired regon of the S-plane for two...
DO THIS ASAP!!!!!!! PART A) OPEN LOOP DYNAMICS OF A SYSTEM IS GIVEN AS) Y"(t)-3y'(t)+2y(t)=x(t) X=input...
DO THIS ASAP!!!!!!!
PART A) OPEN LOOP DYNAMICS OF A SYSTEM IS GIVEN AS)
Y"(t)-3y'(t)+2y(t)=x(t) X=input y=input
FIND K1 AND K2 TO HAVE S1=-1 , S2=-3 AS POLES OF THE CLOSED LOOP
SYSTEM
BOX1[ g(s)] ;BOX2[K1S+K2]
B) FIND THE OVERSHOOT (MP) OF THE FOLLOWING CLOSED LOOP SYSTEM
TO A STEP RESPONSE INPUT
C/R= (S+0.1)/(S^2+1.4s+1)
pen lop dynami'ts af a ststem isgvin e output Poles t the closed tovp system. Find k n d kz to have S -1 KIS+K2 tosed...
A unity feedback system is shown in Fig. 1. The closed-loop transfer function ?(?) of this...
A unity feedback system is shown in Fig. 1. The closed-loop
transfer function ?(?) of this system is given as
?(?)=?1?4+2?3+(?2+1)?2+?2?+?1.
a) (20%) Using Routh-Hurwitz criteria, find expression (in
terms of ?1 and ?2) and range of value of ?1 and ?2 such that the
above system is stable.
b) (4%) It is desired to achieve steady-state error of less
than 0.3 with a unit ramp input. Find an additional constrain in
terms of ?1 and ?2 such that the...
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...
consider the system X(t) = ax(1) + bu(t) with a = 0.001,b= 1,x(0) = 5. (a)...
consider the system
X(t) = ax(1) + bu(t) with a = 0.001,b= 1,x(0) = 5. (a) Simulate this system using the Matlab command initial (b) Now use u(t) = -kx(t) where k is found as the optimal gain by minimizing the performance index J= ax (1) + ru (1) dt Use q=1, r=1 to simulate this system.
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...
Problem 5. Given the system in state equation form, x=Ax + Bu where (a) A=10-3 01, B=10 0 0-2 (b)...
Problem 5. Given the system in state equation form, x=Ax + Bu where (a) A=10-3 01, B=10 0 0-2 (b) A=10-2 01,B=11 Can the system be stabilized by state feedback u-Kx, where K [k, k2 k3l?
Problem 5. Given the system in state equation form, x=Ax + Bu where (a) A=10-3 01, B=10 0 0-2 (b) A=10-2 01,B=11 Can the system be stabilized by state feedback u-Kx, where K [k, k2 k3l?
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...
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....
The parameters are as follows k=0.1,a=1.00,b=1,c=1.0,d=25,w_1=20,w_2=25,Kv=50 e(t) r(t) e (t) G(s) Figure 1: Feedback...
The parameters are as follows
k=0.1,a=1.00,b=1,c=1.0,d=25,w_1=20,w_2=25,Kv=50
e(t) r(t) e (t) G(s) Figure 1: Feedback control system A pulley and belt transmission has a linearized relationship between the driven pulley angle e (t) in degrees and the input torque u(t) in Newton meters given by the following differential equation du(t) dt 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....
Consider the system shown below where the velocity feedback control is utilized. Determine K and Kh...
Consider the system shown below where the velocity feedback control is utilized. Determine K and Kh so that the following specifications are satisfied: 1. Damping ratio of the closed loop system is 0.5 2. Settling time of the closed loop system (according to the 4T criteria) is less than 2s 3. Steady-state error for a unit ramp input is less than or equal to 0.02. R(s) C(s) 2s +1
3. Consider a system with the following state equation h(t)] [0 0 21 [X1(t) [x1(t) y(t) [0.1 0 0.1x2(t) X3(t) The unit step response is required to have a settling time of less than 2 seconds and a percent overshoot of less than 5%. In addition a zero steady-state error is needed. The goal is to design the state feedback control law in the form of u(t) Kx(t) + Gr(t) (a) Find the desired regon of the S-plane for two...
DO THIS ASAP!!!!!!!
PART A) OPEN LOOP DYNAMICS OF A SYSTEM IS GIVEN AS)
Y"(t)-3y'(t)+2y(t)=x(t) X=input y=input
FIND K1 AND K2 TO HAVE S1=-1 , S2=-3 AS POLES OF THE CLOSED LOOP
SYSTEM
BOX1[ g(s)] ;BOX2[K1S+K2]
B) FIND THE OVERSHOOT (MP) OF THE FOLLOWING CLOSED LOOP SYSTEM
TO A STEP RESPONSE INPUT
C/R= (S+0.1)/(S^2+1.4s+1)
pen lop dynami'ts af a ststem isgvin e output Poles t the closed tovp system. Find k n d kz to have S -1 KIS+K2 tosed...
A unity feedback system is shown in Fig. 1. The closed-loop
transfer function ?(?) of this system is given as
?(?)=?1?4+2?3+(?2+1)?2+?2?+?1.
a) (20%) Using Routh-Hurwitz criteria, find expression (in
terms of ?1 and ?2) and range of value of ?1 and ?2 such that the
above system is stable.
b) (4%) It is desired to achieve steady-state error of less
than 0.3 with a unit ramp input. Find an additional constrain in
terms of ?1 and ?2 such that the...
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...
consider the system
X(t) = ax(1) + bu(t) with a = 0.001,b= 1,x(0) = 5. (a) Simulate this system using the Matlab command initial (b) Now use u(t) = -kx(t) where k is found as the optimal gain by minimizing the performance index J= ax (1) + ru (1) dt Use q=1, r=1 to simulate this system.
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...
Problem 5. Given the system in state equation form, x=Ax + Bu where (a) A=10-3 01, B=10 0 0-2 (b) A=10-2 01,B=11 Can the system be stabilized by state feedback u-Kx, where K [k, k2 k3l?
Problem 5. Given the system in state equation form, x=Ax + Bu where (a) A=10-3 01, B=10 0 0-2 (b) A=10-2 01,B=11 Can the system be stabilized by state feedback u-Kx, where K [k, k2 k3l?
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....
The parameters are as follows
k=0.1,a=1.00,b=1,c=1.0,d=25,w_1=20,w_2=25,Kv=50
e(t) r(t) e (t) G(s) Figure 1: Feedback control system A pulley and belt transmission has a linearized relationship between the driven pulley angle e (t) in degrees and the input torque u(t) in Newton meters given by the following differential equation du(t) dt 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....
Consider the system shown below where the velocity feedback control is utilized. Determine K and Kh so that the following specifications are satisfied: 1. Damping ratio of the closed loop system is 0.5 2. Settling time of the closed loop system (according to the 4T criteria) is less than 2s 3. Steady-state error for a unit ramp input is less than or equal to 0.02. R(s) C(s) 2s +1
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