Root Locus. E(s) K. R(s) C(s) 1 s(s+a) Consider the closed loop transfer function:



Similar documents
Understanding Poles and Zeros

ECE 3510 Final given: Spring 11

MATLAB Control System Toolbox Root Locus Design GUI

Stability of Linear Control System

Engineering Sciences 22 Systems Summer 2004

Chapter 3 AUTOMATIC VOLTAGE CONTROL

Σ _. Feedback Amplifiers: One and Two Pole cases. Negative Feedback:

ROUTH S STABILITY CRITERION

G(s) = Y (s)/u(s) In this representation, the output is always the Transfer function times the input. Y (s) = G(s)U(s).

Chapter Eight Root Locus Control Design. 8.3 Common Dynamic Controllers

Bode Diagrams of Transfer Functions and Impedances ECEN 2260 Supplementary Notes R. W. Erickson

Positive Feedback and Oscillators

Introduction to Control Systems

Lecture 9. Poles, Zeros & Filters (Lathi 4.10) Effects of Poles & Zeros on Frequency Response (1) Effects of Poles & Zeros on Frequency Response (3)

Algebra 2 Chapter 1 Vocabulary. identity - A statement that equates two equivalent expressions.

DC motors: dynamic model and control techniques

ab = c a If the coefficients a,b and c are real then either α and β are real or α and β are complex conjugates

First, we show how to use known design specifications to determine filter order and 3dB cut-off

Process Dynamics, Operations, and Control Lecture Notes - 11 Lesson 11. Frequency response of dynamic systems.

Section 9.5: Equations of Lines and Planes

MAC Learning Objectives. Module 10. Polar Form of Complex Numbers. There are two major topics in this module:

S-DOMAIN ANALYSIS: POLES, ZEROS, AND BODE PLOTS

10.5. Click here for answers. Click here for solutions. EQUATIONS OF LINES AND PLANES. 3x 4y 6z 9 4, 2, 5. x y z. z 2. x 2. y 1.

19 LINEAR QUADRATIC REGULATOR

Analysis of Common-Collector Colpitts Oscillator

CIRCLE COORDINATE GEOMETRY

Introduction to Bode Plot

THE COMPLEX EXPONENTIAL FUNCTION

Using the Impedance Method

1.2 Second-order systems

Graphs of Polar Equations

Chapter 29: Magnetic Fields

Part IB Paper 6: Information Engineering LINEAR SYSTEMS AND CONTROL Dr Glenn Vinnicombe HANDOUT 3. Stability and pole locations.

CHAPTER FIVE. 5. Equations of Lines in R 3

Estimated Pre Calculus Pacing Timeline

Graphing Rational Functions

13.4 THE CROSS PRODUCT

Trigonometric Functions: The Unit Circle

2.2 Magic with complex exponentials

88 CHAPTER 2. VECTOR FUNCTIONS. . First, we need to compute T (s). a By definition, r (s) T (s) = 1 a sin s a. sin s a, cos s a

The Vector or Cross Product

Chapter 9: Controller design

Introduction to Complex Numbers in Physics/Engineering

Chapter 6 Circular Motion

2 Session Two - Complex Numbers and Vectors

UNIVERSITY OF CALIFORNIA AT BERKELEY College of Engineering Department of Electrical Engineering and Computer Sciences. EE105 Lab Experiments

Circle Name: Radius: Diameter: Chord: Secant:

Transmission Lines. Smith Chart

Agilent AN 154 S-Parameter Design Application Note

South Carolina College- and Career-Ready (SCCCR) Pre-Calculus

Week 13 Trigonometric Form of Complex Numbers

Introduction to the Smith Chart for the MSA Sam Wetterlin 10/12/09 Z +

1.3 LINEAR EQUATIONS IN TWO VARIABLES. Copyright Cengage Learning. All rights reserved.

EECE 460 : Control System Design

Solutions to Exercises, Section 5.1

Math 241, Exam 1 Information.

n 2 + 4n + 3. The answer in decimal form (for the Blitz): 0, 75. Solution. (n + 1)(n + 3) = n lim m 2 1

Progettazione Funzionale di Sistemi Meccanici e Meccatronici

Review B: Coordinate Systems

Mechanics lecture 7 Moment of a force, torque, equilibrium of a body

F B = ilbsin(f), L x B because we take current i to be a positive quantity. The force FB. L and. B as shown in the Figure below.

Section 9.1 Vectors in Two Dimensions

Angles and Quadrants. Angle Relationships and Degree Measurement. Chapter 7: Trigonometry

Controller Design in Frequency Domain

1.2 GRAPHS OF EQUATIONS. Copyright Cengage Learning. All rights reserved.

Solutions to Homework 10

Homework 1 1. Calculus. Homework 1 Due Date: September 26 (Wednesday) x x 280. R = x. C = 95x

A synonym is a word that has the same or almost the same definition of

EE 402 RECITATION #13 REPORT

Lecture 8 : Coordinate Geometry. The coordinate plane The points on a line can be referenced if we choose an origin and a unit of 20

The basic cascode amplifier consists of an input common-emitter (CE) configuration driving an output common-base (CB), as shown above.

Expression. Variable Equation Polynomial Monomial Add. Area. Volume Surface Space Length Width. Probability. Chance Random Likely Possibility Odds

In mathematics, there are four attainment targets: using and applying mathematics; number and algebra; shape, space and measures, and handling data.

CHAPTER 2 Estimating Probabilities

2.161 Signal Processing: Continuous and Discrete Fall 2008

MAT 1341: REVIEW II SANGHOON BAEK

MATHS LEVEL DESCRIPTORS

Enhancing Classical Controls Education via Interactive GUI Design

POLYNOMIAL FUNCTIONS

Astromechanics Two-Body Problem (Cont)

EDUMECH Mechatronic Instructional Systems. Ball on Beam System

12.4 UNDRIVEN, PARALLEL RLC CIRCUIT*

Largest Fixed-Aspect, Axis-Aligned Rectangle

DEFINITION A complex number is a matrix of the form. x y. , y x

Bending Stress in Beams

TRIGONOMETRY Compound & Double angle formulae

Eðlisfræði 2, vor 2007

5.3 The Cross Product in R 3

Loop Analysis. Chapter Introduction

Optimal Design of α-β-(γ) Filters

Algebra 2 Year-at-a-Glance Leander ISD st Six Weeks 2nd Six Weeks 3rd Six Weeks 4th Six Weeks 5th Six Weeks 6th Six Weeks

LINEAR EQUATIONS IN TWO VARIABLES

ε: Voltage output of Signal Generator (also called the Source voltage or Applied

Chapter 3: Analysis of closed-loop systems

Parametric Equations and the Parabola (Extension 1)

Mathematics. ( : Focus on free Education) (Chapter 5) (Complex Numbers and Quadratic Equations) (Class XI)

x 2 + y 2 = 1 y 1 = x 2 + 2x y = x 2 + 2x + 1

2312 test 2 Fall 2010 Form B

4 The Rhumb Line and the Great Circle in Navigation

Transcription:

Consider the closed loop transfer function: Root Locus R(s) + - E(s) K 1 s(s+a) C(s) How do the poles of the closed-loop system change as a function of the gain K? The closed-loop transfer function is: The characteristic equation: Closed-loop poles:

Root Locus When the gain is 0, the closed loop poles are the openloop poles Roots are real and distinct and for a positive a, in the left half of the complex plane. Two coincident poles (Critically damped response) Roots are complex conjugate with a real part of a/2. Im K=0 X K=0 X 0 Re

Root Locus The locus of the roots of the closed loop system as a function of a system parameter, as it is varied from 0 to infinity results in the moniker, Root-Locus. The root-locus permits determination of the closed-loop poles given the open-loop poles and zeros of the system. For the system: R(s) + - E(s) G(s) C(s) H(s) the closed loop transfer function is: The characteristic equation:

Root Locus when solved results in the poles of the closed-loop system. The characteristic equation can be written as: Since G(s)H(s) is a complex quantity, the equation can be rewritten as: Angle criterion: Magnitude criterion: The values of s which satisfy the magnitude and angle criterion lie on the root locus. Solving the angle criterion alone results in the root-locus. The magnitude criterion locates the closed loop poles on the locus.

Root Locus Often the open-loop transfer function G(s)H(s) involved a gain parameter K, resulting in the characteristic equation: Then the root-loci are the loci of the closed loop poles as K is varied from 0 to infinity. To sketch the root-loci, we require the poles and zeros of the open-loop system. Now, the angle and magnitude criterion can be schematically represented as, for the system:

Root Locus s Im Im A 2 θ 2 X -p 2 θ 2 X -p 2 A 3 A 1 s A 2 A 4 B 1 φ 1 θ 4 θ 1 X X -p 4 -z 1 -p 1 Re A 4 B1 A 1 θ 1 θ X 4 φ 1 X -p 4 -z 1 -p 1 Re A 3 θ 3 X -p 3 θ 3 X -p 3

Consider the system: R(s) + - E(s) Root Locus (Example) C(s) The open loop poles and zeros are: Determine root locus on the real axis: Select a test point on the positive real axis, which indicates that the angle criterion is not satisfied. Consider a test point between 0 and -1, then The angle criterion: indicates that the angle criterion is satisfied.

Consider a test point between -1 and -2, then Root Locus (Example) The angle criterion: indicates that the angle criterion is not satisfied. Consider a test point between -2 and -infinity, then The angle criterion: indicates that the angle criterion is satisfied. Thus, a point on the real axis lies on a locus if number of open-loop poles plus zeros on the real axis to the right of this point are odd.

Root Locus (Example) Asymptotes of the root-loci as s tends to infinity can be determined as follows: Select a test point far from the origin: and the angle criterion is: or, the angle of the asymptotes are: For this example, they are 60 o, -60 o, -180 o. To draw the asymptotes, we must find the point where they intersect the real-axis. Since, the transfer function for a test point s far from the origin permits us to approximate the transfer function as:

Root Locus (Example) The angle criterion for the approximated system is: Substituting, we have Taking the tangent of both sides, we have: which can be written as:

Root Locus (Example) The three equations result is three straight lines shown below, which are the asymptotes, which meet at the point s=-1. Thus, the abscissa of the intersection of the asymptotes and the real-axis is determined by setting the denominator of the approximated transfer function to zero and solving for s. Im -1 Re

Root Locus (Example) The root loci starting from 0 and -1, break away from the real axis as K is increased. The breakaway point corresponds to a point in the s-plane where multiple roots of the characteristic equation occur. Representing the characteristic equation as: We know that f(s) has multiple roots at s = s 1, if Which when substituted into Equation 1, gives us:

Root Locus (Example) Consider the equation: which can be rewritten as: The derivative of K with respect to s gives: Which when set to zero gives the same constraint as before: Therefore, the breakaway point can be determined by setting:

For the current example, we have: Root Locus (Example) The derivative of K with respect to s gives: or Since the breakaway point must lie between 0 and -1, s = -0.4226 corresponds to the actual breakaway point and the corresponding gain is: The gain corresponding to the point s = -1.5774 is: Which belongs to the complementary root-locus.

Root Locus (Example) Locations where the Root-loci crosses the imaginary axis can be determined by substituting s = jω in the characteristic equation as solving for K and s. For the current example, we have or Equating the real and imaginary parts to zero, we have which results in the solutions: Thus, the root locus cross the imaginary axis at

Root Locus (Example) Consider the system with an open-loop transfer function: which has open loop poles at: and a zero at From the rule about existence of root-loci on the real axis, it is clear that to the left of the point s=-2, the entire real axis is part of the root-loci. Since root-loci start at open-loop poles and end at open-loop zeros, we know that the two root-loci which start at the complex open loop poles should break in on the real axis and one of the root-loci should move towards s = -2, and the other towards How does the root locus depart from?

Root Locus (Example) Consider a test point s in the vicinity of the complex open-loop pole p 1 : s θ 1 X -p 1 Im -z 1 φ 1 Re θ 2 X -p 2 The angular contribution of the pole p 2 and the zero z 1 to the test point s can be considered to be the same as the angle made by the lines connecting the pole p 2 and zero z 1 to the pole p 1 (if the test point is close to p 1 ). Then, the angle of departure t1 is given by the angle criterion:

Determine break-in point of the root-loci: Root Locus (Example)

Root Locus (sketching rules) Rule 1: Root locus is symmetric about the real axis roots of characteristic equations are either real or complex conjugates Can draw upper half plane only, although typically full s-plane loci are sketched Rule 2: Each branch of the root locus originates at the open-loop pole with k=0, and terminates either at an open-loop zero or at infinity as k tends to infinity. Characteristic Equation: When k=0, poles at: which are open-loop poles Rewrite Characteristic Equation: When k-> infinity, poles at: which are open-loop zeros -m branches of the root loci terminate at open-loop zeros - remaining (n-m) branches go to infinity along asymptotes as k-> infinity

Root Locus (sketching rules) Rule 3: A point on the real axis lies on a locus if number of open-loop poles plus zeros on the real axis to the right of this point are odd. Rule 4: The (n-m) branches of the root loci which tend to infinity do so along straight line asymptotes whose angles are: Rule 5: The asymptotes cross the real axis at a point given by:

Root Locus (sketching rules) Rule 6: Break points (points at which multiple roots of the characteristic equation occur) of root locus are solutions of dk/ds = 0. Rule 7: The angle of departure from an open-loop pole is given by: where φ is the net angle contribution at the pole of all other open-loop poles and zeros. Similarly, the angle of arrival at an open-loop zero is given by: where φ is the net angle contribution at the pole of all other open-loop poles and zeros. Angle of departure from real open-loop pole or angle of arrival at real open-loop zero is always 0 or π. Rule 8: The points at which branches cross the imaginary axis can be determined by letting s=jω in the characteristic equation.

Effect of addition of poles: Control Design using Root Locus

Control Design using Root Locus Effect of addition of zeros:

Control Design using Root Locus Consider the open-loop system with a transfer function: The root locus of this system is: The close loop transfer function is: with closed loop poles of: It is desired to modify the closed-loop poles so that the closed loop poles have a natural frequency of 4 rad/sec and a damping ratio of 0.5, or which does not lie on the original root-locus. We need a compensator to move the poles.

Control Design using Root Locus Angle criterion requires: Since the angle is 30 less than what it should be, add 30 degree via a zero, or a PD controller k(s+z). The location of the zero z is selected to satisfy the angle criterion.

Control Design using Root Locus Thus, the zero is located at: The PD controller is k(s+8). The open loop transfer function is: The magnitude criterion is used to determine k: