The Nyquist Stability Criterion - SNS Courseware · The Nyquist Stability Criterion Born in 1889 in...

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The Nyquist Stability CriterionBorn in 1889 in SwedenDied in 1976, USAYale PhD, 1917Career at Bell Labs138 patentsNyquist diagram,

criterion, sampling theorem

Laid the foundation forinformation theory, datatransmission andnegative feedback theory

Frequency Response Plots

(Review Appendix G in textbook)

)Re()Im(tan

)(Im)(Re|)(|

1

22

ωωφ

ωωω

−=

+=G

Frequency Response Plots

)(tan1/tan

)Re()Im(tan)(

1

1111

ωωωω

ωωωφ −−− −=

−==

1st Ordersystem

Polar Plot or Nyquist Diagram

)1(tantan)Re()Im(tan)( 1

211

ωττωω

ωωωφ −−− =

−−

==KK

2rd system)1()(

+=

τssKsG

Polar Plots and the Nyquist Criterion

• We have seen how to generate polarplots of the frequency response.

• The Nyquist criterion is a way ofinterpreting the polar plot to determinestability

• The frequency response in the entire right-half s- plane with s=-j∞ to s=+j∞is the critical section of the Nyquist contour.

Mapping Contours in the s-Plane

• Nyquist stability criterion based onCauchy theorem on functions of acomplex variable

• Mapping contours1+L(s)=0

in the s-plane.

Mapping Contours in the s-Plane

Closed contours

Conformal mapping (angles are preserved)

F(s)=2s+1

Mapping Contours in the s-Plane

S-plane F(s)-plane

Cauchy’s Theorem: Principle of the Argument

If a contour in the s-plane encircles Z zeros and Ppoles of F(s ) and does not pass through any poles or zeros of F(s ) and the traversal is in the clockwise direction along the contour, the corresponding contour in the F(s)-plane encircles the origin of the F(s)-plane N=Z-P times in the clockwise direction

S-plane F(s)-plane

?N=1-1=0

Illustration of Cauchy’s Theorem

N=Z-P=3-1=2

Illustration of Cauchy’s Theorem

N=Z-P=0-1=-1

The Nyquist CriterionThe Nyquist contour encircles the entire right-half s- plane

For the system to be stable, allzeros (or roots) of F(s ) must lie in the left-hand s-plane.

The number of unstable zeros of F(s) is thus

Where N is the number encirclements of the origin.

When the system is open- loop stable

P=0 and then Z=N

Z=N+P

N=Z-P

The Nyquist Criterion

In practice it is more convenient to consider the mapping

in which case becomes the number of clockwise encirclements of the -1 point.

The Nyquist contour encircles the entire right-half s- plane

Z is unstable zero and P is unstable pole if they are lied withinNyquist contour.

The Nyquist Criterion

1) Open-loop stable plant

A feedback system is stable if and only if the contour in the -plane does not encircle the (-1,0) point.

2) Open-loop unstable plant

A feedback system is stable if and only if, for the contour in the -plane, the number of counterclockwise of the (-1,0) point is equal to the number P of poles of with positive real parts.

Z=N+P For stable system, the closed loop Z=0.

Z=0 => N=0

Z=0 => N=-P

System with Two Real Poles

hence for stability we require Z=N=0,

i.e. the contour must not encircle the -1 point in the GH(s)-plane.

Stable

)11.0)(1(100

)1)(1()(

21 ++=

++=

ssssKsGHττ

x

System with a Pole at the Origin

The Cauchy theorem requiresthat the contour cannot passthrough the pole

Modified or indentedNyquist contour

0>=εR

System with a Pole at the Origin

Small circular detour represented by

varies from

where

for this portion is an infinite semi-circle

going from

and passing through

System with a Pole at the Origin

Portion from

Magnitude is zero when r is infinite

System with a Pole at the Origin

The Cauchy theorem requiresthat the contour cannot passthrough the pole

Modified or indentedNyquist contour

0>=εR

Stable

?

System with Three Poles

System with Three Poles

The system is stable or not depending on the k value.

System with Three Poles

System with Two Poles at the Origin

Angle ofN=2 hence Z=2, i.e. two roots in the RHP

Unstable for all K

System with a Pole in the RHP

P=1, hence we require N=-P=-1for stability.

With

Infinite semicircle in the LHP

With

Two roots in the RHP

System with a Pole in the RHPAdding derivative action

When

Crosses real axis whenStable

System with a Zero in the RHP

-2K

Unstable for K>1/2

Relative Stability

u=-1 when

crosses the real axis at

Ultimate point

Relative Stability and Nyquist Criterion

• Clearly, from the Nyquist criterion thedistance between the (-1,0) point andthe polar plot of the loop transferfunction GH(jω) is a measure of therelative stability of the system

• Note that the (-1,0) point on a Nyquistdiagram corresponds to the 0 dB and -180 degrees on the Bode magnitudeand phase diagrams

Relative Stability• The gain margin is the increase in the

system gain when phase =- that will result in a marginally stable system with intersection of the -1+j0 on the Nyquist diagram

• The phase margin is the amount of phase shift of the GH Nyquist plot at unity magnitude that will result in a marginally stable system with intersection of the -1+j0 point on the Nyquist diagram

0180

Gain MarginThe factor by which the gain at ultimate point can beincreased to reach marginal stability

Expressed in dB:

Reasonable values aregain margins in the range[2 5], or in dB [6 14]dB.

Phase Margin

The phase margin is the difference between and

the phase of the loop at the crossover frequency

Reasonable values are phase margins in the range [30 60] degrees

Gain and Phase Margins on the Bode Diagram

Sensitivity and Nyquist PlotThe radius r of the circle centered at -1 and tangen to L is the reciprocal of the nominal sensitivity peak

Critical point

Effect of Time Delay

• The Nyquist criterion is applicable tonon-rational transfer functions

• A time delay is described by

• It does not introduce additional poles or zeros within the contour

• However delay introduces phase lagand consequently has a destabilizingeffect.

Effect of Time Delay

adds a phase shift

At the crossover frequency

might be sufficient to destabilize the system orto significantly reduce the phase margin

Effect of Time Delay

Phase marginfor delay-freesystem

Delayedsystem isunstable!

System with Delay

Consider the following delayed system:

With a second-order Pade approximation, the delay can be written as

Hence

System with Delay

K = 2.41

System with Delay

K=3

K=2

K=1