Elements of Feedback Control - PowerPoint PPT Presentation

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Elements of Feedback Control

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... omegan, sigma, omegad % plot allowable region for pole location ... One root locus branch comes out of each pole, so there are a total of n branches. – PowerPoint PPT presentation

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Title: Elements of Feedback Control


1
Name_________________
In order to have transient die out, all
closed-loop poles of the system must __in the
LHP, or stable__ Use z, s, wn , and wd to fill
in the spaces below. Settling time is inversely
proportional to ____ s_____ Rise time is
inversely proportional to ____ wn
_____ Percentage overshoot is most directly
determined by ___ z ____ Oscillation frequency
determined by ____ wd _____
2
Prototype 2nd order system
target
3
Settling time
4
Effects of additional zeros
Suppose we originally have
i.e. step response
Now introduce a zero at s -z
The new step response
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Effects
  • Increased speed,
  • Larger overshoot,
  • Might increase ts

7
When z lt 0, the zero s -z is gt 0, is in the
right half plane. Such a zero is called a
nonminimum phase zero. A system with nonminimum
phase zeros is called a nonminimum phase system.
Nonminimum phase zero should be avoided in
design. i.e. Do not introduce such a zero in
your controller.
8
Effects of additional pole
Suppose, instead of a zero, we introduce a pole
at s -p, i.e.
9
L.P.F. has smoothing effect, or averaging effect
Effects
  • Slower,
  • Reduced overshoot,
  • May increase or decrease ts

10
Matlab program template
enter plant transfer function Gp(s) nump .
denp. enter desired closed loop step
response specification you may allow both
uppper and lower limits convert from specs
to zeta, omegan, sigma, omegad plot
allowable region for pole location obtain
controller transfer function for now make C(s)
1 numc1 denc1 obtain closed loop transfer
function from Gp(s) and C(s) numcl
dencl obtain closed-loop step response
compute actual step response specs, using
your program from last week are they
good? compute the actual closed-loop poles,
place x at those locations are they in
the allowable region?
11
Root locus
  • A technique enabling you to see how close-loop
    poles would vary if a parameter in the system is
    varied
  • Can be used to design controllers or tuning
    controller parameters so as to move the dominant
    poles into the desired region

12
  • Recall step response specs are directly related
    to pole locations
  • Let p-sjwd
  • ts proportional to 1/s
  • Mp determined by exp(-ps/wd)
  • tr proportional to 1/p
  • It would be really nice if we can
  • Predict how the poles move when we tweak a system
    parameter
  • Systematically drive the poles to the desired
    region corresponding to desired step response
    specs

13
Root Locus
k s(sa)
y
e
r
Example

-
Two parameters k and a. would like to know how
they affect poles
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22
The root locus technique
  • Obtain closed-loop TF and char eq d(s) 0
  • Rearrange terms in d(s) by collecting those
    proportional to parameter of interest, and those
    not then divide eq by terms not proportional to
    para. to get
  • this is called the root locus equation
  • Roots of n1(s) are called open-loop zeros, mark
    them with o in s-plane roots of d1(s) are
    called open-loop poles, mark them with x in
    s-plane

23
  1. The o and x marks falling on the real axis
    divide the real axis into several segments. If a
    segment has an odd total number of o and/or x
    marks to its right, then n1(s)/d1(s) evaluated on
    this segment will be negative real, and there is
    possible k to make the root locus equation hold.
    So this segment is part of the root locus. High
    light it. If a segment has an even total number
    of marks, then its not part of root locus. For
    the high lighted segments, mark out going arrows
    near a pole, and incoming arrow near a zero.

24
  • Let npolesorder of system, mzeros. One root
    locus branch comes out of each pole, so there are
    a total of n branches. M branches goes to the m
    finite zeros, leaving n-m branches going to
    infinity along some asymptotes. The asymptotes
    have angles (p 2lp)/(n-m). The asymptotes
    intersect on the real axis at

25
  • Imaginary axis crossing
  • Go back to original char eq d(s)0
  • Use Routh criteria special case 1
  • Find k value to make a whole row 0
  • The roots of the auxiliary equation are on jw
    axis, give oscillation frequency, are the jw axis
    crossing points of the root locus
  • When two branches meet and split, you have
    breakaway points. They are double roots. d(s)0
    and d(s) 0 also. Use this to solve for s and k.
  • Use matlab command to get additional details of
    root locus
  • Let num n1(s)s coeff vector
  • Let den d1(s)s coeef vector
  • rlocus(num,den) draws locus for the root locus
    equation
  • Should be able to do first 7 steps by hand.
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