Exam 2 Flashcards

1
Q

The zeros of the characteristic equation change as ________ changes

A

K

Lecture 13: Routh Stability Criterion

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2
Q

Routh Stability Criterion (definition)

A

A method of obtaining information about the location of the roots of a polynomial without actually solving for the roots

Lecture 13: Routh Stability Criterion

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3
Q

What are the tests for Routh Stability?

A
  1. Are all of the coefficients of the characteristic polynomial positive (and present)?
  2. Are all the elements in the 1st column of the Routh array POSITIVE?

Lecture 13: Routh Stability Criterion

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4
Q

In a Routh Array, ________________ gives the number of poles of the characteristic equation that are on the right side of the S-plane.

A

The number of sign changes of the elements in the 1st column

Lecture 13: Routh Stability Criterion

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5
Q

Steps to analyzing system using a Routh Array

A
  1. Find the transfer function of the closed loop system
  2. Re-arrange characteristic equation to the form:
    1s^n + a_1s^(n-1) + … + a_n-1s^1+a_ns^0
  3. Apply test 1
  4. Form Routh Array
  5. Apply test 2

Lecture 13: Routh Stability Criterion

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6
Q

Two assumptions for this class

A
  1. The plant and controller are LTI systems
  2. Single input - single output (SISO) systems

Lecture 14: Basic Eqn.s of Control

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7
Q

Basic concerns of controls engineers

A
  1. Stability
  2. Tracking
  3. Regulation
  4. Sensitivity

Our mission is to create an appropriate control signal to drive the system

Lecture 14: Basic Eqn.s of Control

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8
Q

Types of control

A
  1. Tracking: cause the output to follow the reference as closely as possible
  2. Regulation: keep the error as small as possible

Lecture 15: Conflicting Tradeoffs

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9
Q

What is the purpose of the Root Locus?

A

Determines

  1. The values of K at which the system is stable
  2. How the time response changes as K changes

AKA it is a guide to how poles change as K changes

Lecture 15: Conflicting Tradeoffs

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10
Q

The Root Locus can be thought of as…

A

A method for inferring the dynamic properties of the closed loop system a K changes

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11
Q

The value of s is a closed-loop pole of a closed loop system if:

A
  1. | KG(s)H(s) | = 1
  2. < KG(s)H(s) = (2k+1)180deg

Lecture 15: Conflicting Tradeoffs

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12
Q

Characteristic polynomial form for using Root Locus

A
1+KL(s)
where L(s) = b(s)/a(s) for a(s)+K*b(s)

Lecture 16: Root Locus

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13
Q

Root Locus Rules

A
  1. The n branches of the locus start at the poles of L(s) when K=0, and the m branches end on the zeros of L(s) when K = infinity.
  2. The loci are on the real axis to the left of an odd number of poles and zeros
  3. For large s and K, n-m branches of the loci are asymptotic to lines at angles p radiating out from the center point s = alpha on the real axis
    p = (180 + 360(l-1)) / (n-m), l = 1, 2, …, n-m
    anchor point = alpha = [sum(pi) - sum(zi)] / (n-m)

Lecture 16: Root Locus

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14
Q

For the Root Locus, what does changing K mean?

A
  1. The poles change
  2. Consequently, the step response (i.e. time response) changes

Lecture 16: Root Locus

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15
Q

Integral Controller Expression

A

Ki/s

Lecture 17: PI Controller

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16
Q

What is the purpose of an integral controller?

A

Minimize the steady-state tracking error and the steady-state output response to disturbances
AKA: Remove the steady state error

Lecture 17: PI Controller

17
Q

When should you use a PD controller?

A

When the root locus does not fit the time domain response you need

Lecture 18: PD Controller

18
Q

Derivative Controller Expression

A

Kd*s

Lecture 18: PD Controller

19
Q

What is the goal of derivative feedback?

3 things

A
  1. Improve closed loop system stability
  2. Speed up the transient response
  3. Reduce overshoot

Lecture 18: PD Controller

20
Q

Control Law for PD Controller

A

Trend of error:
U(t) = Kd*de(t)/dt
Increasing control amplifies error/noise

Lecture 18: PD Controller

21
Q

An extra zero may….

A

Increase the overshoot of the step response by a little

Lecture 18: PD Controller

22
Q

To reduce the steady state error to constant reference and disturbance inputs use a(n) ___________ controller

A

Integral

23
Q

To speed up the transient response and reduce overshoot use this type of controller:

A

Derivative

24
Q

“anticipatory term”

A

Derivative

25
Q

Gain Margin, GM

A

The change in the open-loop gain required at 180deg phase shift to make the closed loop system unstable
Expressed in dB

26
Q

Phase Margin, PM

A

The change in open-loop phase shift required at unity gain to make the closed-loop system unstable

27
Q

Stability: Typically an open-loop system is stable in closed-loop if…

A

The open-loop magnitude frequency response has a gain of less than 0dB at the frequency where the phase frequency response is 180

28
Q

Percent overshoot is reduced by…

A

Increasing the phase margin

29
Q

Speed of Response is increased by….

A

Increasing the bandwidth

30
Q

Steady-state error is improved by

A

Increasing the low-frequency magnitude response (even if the high-f response is attenuated)

31
Q

A _____ PM is required for stability

A

positive

32
Q

How to find GM

A
  1. Find where phase crosses -180deg
  2. Follow the frequency up to magnitude plot
  3. GM = magnitude at that point-0dB; log(w)