EECE 460 Homework, Spring 2008
American University of Beirut · Control Systems · 4 pages
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B-5-1, Time constant = 0.25 min. The steady-state error is 2.5 degrees.
ar a pe Ma Sl TANS SS rere were
B-5-2. Rise time = 2.42 sec
Peak time = 3.63 sec
Maximum overshoot = 0.163
Settling time = 8 sec (2 % criterion)
i A A Po AE
B-5-3. The maximm overshoot of 5% corresponds to $= 0.69. Hence
2 2
4, = = = 2,
airway) 2.90 dad [sec
Cy) . _K(Tst/)
Ro) Ist KTS+K
Since T = 3, K/J = 2/9, we have
oe A)
RO) s*+(4)38 +s
Hence, 2 $ Wy = 6/9 and W,? = 2/9. Thus
$=0.907
rr er a
B-S18. For the given system we have
<a K
RG) St pease KAS +K
Nota that
Kasay = 67 = ff
Since
we obtain 25am - 2tkKk
BXOPKRY HBtKK AR A+ GR
Thus
fk =e.2287
—=--__-- = — +
a
5-12:
% ***** Unit-step response *****
num = [0 0 10];
den =[1 2 10];
t = 0:0.02:10;
step(num,den,t)
gri
title("Unit-Step Response’)
xlabel("t Sec’)
ylabel{'c(t)’)
% ***** Unit-ramp response *****
- numer = [0 00 10);
denr = [1 2 10 O};
c= step(numr,denr,t);
plotit.e, =" tet, "=")
Stle("Unit-Ramp Response’)
xlabel("t Sec’)
ylabel('c(t)')
% ***** Unit-impulse response *****
impulse{num,den,t)
gr
title("Unit-impulse Response’)
xlabel('t Sec’)
ylabel("c(t)")
The unit-step response curve is shown below. The unit-ramp response curve and
-unit-impulse response curve are shown on the next page.
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