Chapter 2 System IInd Order Responses
Transcript of Chapter 2 System IInd Order Responses
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Chapter 2 (page#119)
Continuous-TimeSystem Responses
2.3 Response of Second-Order Systems
2.5 Stability Testing
2.4 Higher- Order System Response
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System Response
First-order system time response
transient
dc steady-state
Second-order system time response
transientdc steady-state
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Ist & IInd order systems if stable:
the forced response is the steady-state
responseand the natural response is the transient
response
For unstable responses, "steady-state" and"transient" are meaningless
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2.3 (p 126) RESPONSE OF SECOND-ORDER SYSTEMS
)......(asas
b
)s(R
)s(C)s(G 174
012
0
The Standard form of the second-order transfer function is given by:
)......(ss)s(R
)s(C)s(G
nn
n 1842 22
2
, the damping ratio, will determine how much the systemoscillates as the response decays toward steady state.
n, the undamped natural frequency (natural frequency) , willdetermine how fast the system oscillates during any transientresponse.
Note: All system chracteristics of the 2nd-order system are
functions of only and n.
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22
2
2 nn
n
ss)s(R
)s(C
)s(G
)unityisdcgain()(R
)(C)(G 1
0
00
G(0): DC gain of the system, will determine the size of steady
state response when the input settles out to a constant value.
We will also consider 2nd-order systems with other than unity
gain and with numerator other than a constant.
2.3 (p 126) RESPONSE OF SECOND-ORDER SYSTEMS..cont
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Unit-step response for standard Second-0rder system
)s(R)s(G)s(C R(s) C(s)22
2
2 nn
n
ss
sss)s(C
nn
n 1
222
2
s)s(G)s(C1
)tsin(e)t(c ntn
11
Assume poles of G(s) are complex, taking inverse LLT
21
1tan
n)(constatntTime
1
ns )T(meSettlingTi
44
usoidesindampedoffrequencyn
Step response R(s) = A/s = 1/s unit step response
G(s)
2.3 (p 126) RESPONSE OF SECOND-ORDER SYSTEMS..cont
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Three cases:
Overdamped case: >1, two real
distinct polesUnderdamped case:
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4 cases to be considered
Case 1: Distinct real roots
tsts ecectx
ss
2
2
1
1
21
)(
Case 2: Equal roots & real
stst tecectx
sss
21
21
)(
Case 3: Imaginary roots
tktktx
ecectx
js
tjtj
cossin)(
)(
21
21
Case 4: Complex conjugate roots
tktketx
js
t
cossin)( 21
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>1Distinct
real roots
Timeconstant () ForcingFunction and n
Forcing
Function
=1
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>1
=1
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3
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4
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Step Response
t
)1(
)2(
)(c
rt
pt
st
rt
dt
pMovershoot
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Exponential decay generated by real
part of the complex pole pair
Exponential decay
generated by real
part of the complex
pole pair (=n)
Sinusoidal oscillation
generated by imaginary
part of the complex pole
pair
C(t)
t
)tsin(e)t(c ntn
11
-=-n n
jd
-jd
S-Plan
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t
)1(
)2(
)(c
rt
pt
st
rt
dt
pMovershoot
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P bl 2
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40012
4002
ss
)s(G)a(
Problem
90090
9002
ss
)s(G)b(
22530
2252
ss
)s(G)c(
625
6252
s
)s(G)d(
t.t.
CeBeA)t(c46115478
21 /t/t teCBeA)t(c
)tcos(eBA)t(c ntn
)tcos(BA)t(c 25
)t.cos(eBA)t(ct
08196
21 /t/t CeBeA)t(c
tt teCBeA)t(c 1515
21
22
2
2 nn
n
ss)s(G
N t
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1. The impulse response ofany system does give an indication of the nature of
the initial-condition (IC) response, and thus the transient response, of the system.
3. An Initial condition excitation of a Higher-order system cannot be modeled as
simply as that of the first-order system.
2. An Initial condition on a first-order system can be modeled as an impulse
function input
4. The unit-impulse response of the II-order system is given by the equation:
).(responseimpulse.....tsine)t(c ntn n 254
2
2
22 n
n
ns)t(c -1
).(responsestepUnit).....tsin(e)t(c ntn 20411
Equation 4.25 is the derivative of equation 4.20
5. The impulse response of the second order system can also be considered to
be the response to certain initial conditions, with r(t)=0
Note:-
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Third-order systems (Higher Order System)
Consider one real pole plus a pair ofcomplex conjugate poles
Complex poles dominant (close toorigin), real pole non-dominant
or
Real pole dominant, complex poles
non-dominant
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Complex poles dominant:
approximate as secon-dordersystem
Real pole dominant:
approximate as first-order system
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All three poles dominant:
approximation difficult
Complex conjugate poles
Dominant:zero tends to minimize
effect of nearby real pole
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Real pole dominant,
zeros tend to minimize
effects of nearby poles
Unstable due to rhp pole,
nearby zero is not usefulin canceling pole
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Lhp zero will amplify overshoot
Stable system, rhp zero can
give response that starts inopposite direction from the
steady-state resp
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X
S = -a0
Pole =1/=-a0
Characteristics
Equation
X
S = -a0
Pole =1/=-a0X
S = -a0
Pole =1/=-a0