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Cheat Sheet II - Feedback Control Design | EE 571, Study notes of Electrical and Electronics Engineering

Material Type: Notes; Class: FEEDBACK CONTROL DESIGN; Subject: Electrical Engineering; University: University of Kentucky; Term: Unknown 1989;

Typology: Study notes

Pre 2010

Uploaded on 10/01/2009

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EE571 Cheat Sheet II
Root Locus: Let KGH K sbs ...
sas ...
mm1
nn1
=++
++
be the open-loop transfer function.
Angle Condition: A point s1 is on the R.L. if GH(s1) = 180° x (odd number)
Magnitude Condition: If a point s1 lies on the R.L., then the value of K can be found from |KGH(s1)| = 1
10 rules:1. Starts @ open loop poles @ K=0
2. Ends @ open loop zeroes @ K=
3. # of branches = n
4. R.L. is symmetric WRT σ-axis and any other axis about which the open-loop pole zero configuration is symmetric
5. of asymptotes = 180° (odd #)/(n-m)
6. asymptotes are centered at σ = (b-a)/(n-m)
7. R.L. exists at a pt. on σ-axis if # of poles and zeroes of GH to the right is odd
8. To find angle of departure - draw a pt. very close to pole or zero and use condition
9. Use Routh array to find pt. where R.L. crosses jω-axis
10. Break-away and break-in pts. @ K/s = 0
Root Locus Compensation: Gc(s1) = angle of deficiency = 180° x (odd #) - GH|desired poles; GPID = Ki/s + Kp + Kds
Error Analysis: (Valid for unity-feedback with closed loop system stable):
KlimG(s)
ps0
= K limsG(s)
vs0
= K lims G(s)
as0
2
= ess| 1/ (1 K )
step p
=+ ess| 1/K
ramp v
= ess| 1 / K
parabola a
=
Routh Array: Check the RHP roots of b s b s b s ... b s b 0
nnn1n1 n2n2 10
+++++=
Frequency Response Methods:
Mapping Theorem: Let F(s) be a ratio of two polynomials in s. Choose a
closed contour and map it into the F(s) - plane. Then, the number of
encirclements the mapped contour makes about the origin in the F(s)-plane
(in the same direction as the original contour), in N=Z-P where Z= # of
zeroes of F(s) enclosed by the original contour and P = # of poles of F(s)
enclosed by the original contour
Decibel: 20log(||)
gain margin = 1/|GH(jωcp)| where GH(jωcp) = -180° phase margin = 180°+GH(jωcg) where |GH(jωcg)| = 1 or 0 dB
Conversion Factors: 2 + j= 5 26.6 3 + j = 2 30 1+ j= 2 45 1+ j 3 = 2 60 1+ j2 = 5 63.4
ooo o o
∠∠∠∠;;; ;
1 = 0 dB 2 = 6 dB 3 = 9.5 dB 5 = 14 dB 8 = 18 dB
Lead Compensation Lag Compensation
Gs K Ts
Ts
cc
()=+
+
1
1
α
0 < α < 1 GsK Ts
Ts
lag lag
()=+
+
1
1
β
1 <
β
<
Maximum phase: Find ωcgnew such that
sin m
φ
α
α
=
+
1
1 occurs at
ωα
m1/( T)= GH(jωcg) = -180°+ desired pm + fudge factor
Extra gain at ωm= 1/
α
Attenuation at high frequencies = 1/
β
Sensitivity: Sx
y
Y
X
y
xXnom Ynom
=
|,
Observer Equation: xAxBwKyCx
o
^()
^^
=++
s
n
b
n b
n-2 b
n-4 ...
sn-1 b
n-1 b
n-3 b
n-5 ...
sn-2 c
1 c
2 ...
.
: c1
bn1
bn2 bnbn3
bn1
=−−
s1 c2
bn1
bn4 bnbn5
bn1
=−−
s0

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EE571 Cheat Sheet II

Root Locus: Let KGH K

s bs ...

s as ...

m m 1

n n 1

be the open-loop transfer function.

Angle Condition : A point s1 is on the R.L. if ∠GH(s1) = 180° x (odd number)

Magnitude Condition : If a point s1 lies on the R.L., then the value of K can be found from |KGH(s1)| = 1

10 rules :1. Starts @ open loop poles @ K=

  1. Ends @ open loop zeroes @ K=∞
  2. of branches = n

  3. R.L. is symmetric WRT σ-axis and any other axis about which the open-loop pole zero configuration is symmetric
  4. ∠ of asymptotes = 180° (odd #)/(n-m)
  5. asymptotes are centered at σ = (b-a)/(n-m)
  6. R.L. exists at a pt. on σ-axis if # of poles and zeroes of GH to the right is odd
  7. To find angle of departure - draw a pt. very close to pole or zero and use ∠ condition
  8. Use Routh array to find pt. where R.L. crosses jω-axis
  9. Break-away and break-in pts. @ ∂K/∂s = 0

Root Locus Compensation: ∠G (^) c (s1) = angle of deficiency = 180° x (odd #) - ∠GH| desired poles

; G

PID

= K

i

/s + K p

+ K

d

s

Error Analysis: (Valid for unity-feedback with closed loop system stable):

K lim G(s) p

s 0

K lim sG(s) v

s 0

K lim s G(s)

a s 0

2

ess| 1/ (1 K ) step p

= + ess| 1/ K ramp v

= ess| 1/ K parabola a

Routh Array: Check the RHP roots of b s b s b s ... b s b 0 n

n

n 1

n 1

n 2

n 2

1 0

Frequency Response Methods:

Mapping Theorem : Let F(s) be a ratio of two polynomials in s. Choose a

closed contour and map it into the F(s) - plane. Then, the number of

encirclements the mapped contour makes about the origin in the F(s)-plane

(in the same direction as the original contour), in N=Z-P where Z= # of

zeroes of F(s) enclosed by the original contour and P = # of poles of F(s)

enclosed by the original contour

Decibel : 20log(|⋅|)

gain margin = 1/|GH(jω cp

)| where ∠GH(jω cp

) = -180° phase margin = 180°+∠GH(jω cg

) where |GH(jω cg

)| = 1 or 0 dB

Conversion Factors : 2 + j = 5 26.6 3 + j = 2 30 1+ j = 2 45 1+ j 3 = 2 60 1+ j2 = 5 63.

o o o o o

∠ ; ∠ ; ∠ ; ∠ ; ∠

1 = 0 dB 2 = 6 dB 3 = 9.5 dB 5 = 14 dB 8 = 18 dB

Lead Compensation Lag Compensation

G s K

Ts

Ts

c c

0 < α < 1 G s K

Ts

Ts

lag lag

1 < β < ∞

Maximum phase: Find ω cgnew

such that

sin m

φ

α

α

occurs at ω α

m

= 1/ ( T) ∠GH(jω cg

) = -180°+ desired pm + fudge factor

Extra gain at ω m

= 1/ α Attenuation at high frequencies = 1/ β

Sensitivity: S

x

y

Y

X

y

x

Xnom Ynom

,

Observer Equation: x A x Bw K y C x o

^

^ ^

s

n b n

b n-

b n-

s

n- b n-

b n-

b n-

s

n- c 1

c 2

c 1

b n 1

b n 2

b n

b n 3

b n 1

=

− −

− −

s

c 2

b n 1

b n 4

b n

b n 5

b n 1

=

− −

− −

s