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Couplad systom og eguetien y_(A)^()+2zeta omega _(n)y_(A)^()+omega _(n)^(2)y_(A)-(k_(E))/( ho )i=0 (di)/(dt)+(k)/(L)i+(k_(k))/(L)y_(A)=(V)/(L) Structural damping =xi =0.01 omega _(n)^(2)=(k_(eq))/( ho ), set omega _(n)=25(ral)/(s) R=2.5Omega
Couplad systom og eguetien\
y_(A)^()+2\\\\zeta \\\\omega _(n)y_(A)^()+\\\\omega _(n)^(2)y_(A)-(k_(E))/(\\\ ho )i=0\ (di)/(dt)+(k)/(L)i+(k_(k))/(L)y_(A)=(V)/(L)
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Structural damping =\\\\xi =0.01\ \\\\omega _(n)^(2)=(k_(eq))/(\\\ ho ), set \\\\omega _(n)=25(ral)/(s)\ R=2.5\\\\Omega \ k_(v)=0.1\ k_(T)=2.0\ \\\\xi =0.01
\ inductance
L=10
\ a. Obtain the state space representation of the system where the states are
y_(A),y_(A)^(),i
. The\ sensor measures the velocity at the tip,
y_(A)^()
. Check for controllability and observability.\ b. Find the response for the open system. Move
y_(A)
up 1 meter and then let go. Plot the\ results for all the states . ). Make sure that your sampling frequency is high\ enough so that you get a smooth curve. The plot for
y_(A)
should look like the figure below
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