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Page 1: Nonlinear Systems 2nd- Hassan K. Khalil,Ch1,Ch2

NONLINEAR SYSTEMS

Second Edition & ! + . A .

Hassan K. Khalil Michigan State University

Prentice Hall, Upper Saddle River, NJ 07458

Page 2: Nonlinear Systems 2nd- Hassan K. Khalil,Ch1,Ch2

Ubnrl flC~Cltnlogingin.PubUcatlon Dab

Kha. Hlasm K. NmIimar sysrrma I Harsan K. Khllil.--land ed.]

p. 0".

Indudes indw. ISBN 0-13-P8U24-8 1. Nanlincar b r i e r . I . Title.

QA427.K48 19% 003'. 75--dcm 95-45804

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Aquisitima editor: ALICE DWORKIN EditoriPllomductim auocnririm

md in&a dcsign: SHARYN VlTRANO Covo duigmcr: BRUCE KENSELAAR Manulacwring buyer: DONNA SLZLlVAN Supplanmts edtmr: BARBARA MURRAY

819% by Rmuee-HdI. Inc. Stmm & Schusud A Via- Canpmy Upper Saddle River. New Jersey 07458

AU rights mewed. No pan of this bmlr may bc npmduced, in any form a by m y mans , without permission in writing fmn the publisher.

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Printed in the United S u e s of America

Prcnticc-Hall International (UK) Limited. Lmdon Pnntice-Hall of Austnl* Pty. Limited. Sydney Prmtim-Hall Caruda bc.. Tormto Prcntree-Hd Hlrpnoamcncana. S.A . Mer~u , Prcnocc-Hd of Indm P n v w Llmued. New Dch Prmtiee~Hdl of lapan. Inc.. Tokyo Sintan & Schusur Ash Re. 1.d. Sing- Mlton Pmtiee-Hdl do B n d . Ltd... Rlo de Jmcim

Page 3: Nonlinear Systems 2nd- Hassan K. Khalil,Ch1,Ch2

To Petar V. Kokotovit

Page 4: Nonlinear Systems 2nd- Hassan K. Khalil,Ch1,Ch2
Page 5: Nonlinear Systems 2nd- Hassan K. Khalil,Ch1,Ch2

Preface

This text is intended for a first-year graduate-level course on nonlinear systems. It may also he used for self-study or reference by engineers and applied mathe- maticians. It is an outgrowth of my experience in teaching the nonlinear systems course at Michigan State University, East Lansing, several times since 1985. Stu- dents taking this course have had background in electrical engineering, mechanical engineering, or applied mathematics. The prerequisite for the course is a graduate- level course in linear systems, taught at the level of the texts by Cheu [29], DeCarlo [41], Kailath [86], or Rugh [142]. In writing this text, I have assumed the linear systems prerequisite which allowed me not to worry about introducing the concept of a "state" and to refer freely to "transfer functions," "state transition matrices," and other linear system concepts. As for the mathematics background, I have as- sumed the usual level of calculus, differential equations, and matrix theory that any graduate student in engineering or mathematics would have. In one section, I have collected a few mathematical facts which are used throughout the book. I do not assume that the student has previous knowledge of this material hut I expect, with the level of maturity of graduate students, that with the brief account of these facts provided here they should he able to read through the text without difficulty.

I have written the text in such a way that the level ofmathematicalsophistication builds up as we advance from chapter to chapter. This is why the first chapter is written in an elementary context. Actually this chapter could be taught a t senior, or even junior, level courses without difficulty. This is also the reason I have split the treatment of Lyapunov stability into two parts. In Sections 3.1 to 3.3, I introduce the essence of Lyapunov stability for autonomous systems where I do not have to worry about technicalities such as uniformity, class K functions, etc. In Sections 3.4 to 3.6, I present Lyapunov stability in a more general setup that accommodates nonautonomous systems and allows for a deeper look into advanced aspects of stability theory. The level of mathematical sophistication at the end of Chapter 3 is the level that I like to bring the students to, so that they can comfortably read chapters 4 to 13.

There is yet a higher level of mathematical sophistication that is assumed in writing the proofs given in Appendix A. The proofs collected in this appendix are

Page 6: Nonlinear Systems 2nd- Hassan K. Khalil,Ch1,Ch2

not intended for classroom use. They are included to make the text self contained on one hand, and to respond to the need or desire of some students to read these proofs, like students continuing on to conduct Ph.D. research into nonlinear systems or control theory. Those students can continue to read Appendix A in a self-study manner. By the higher level of sophistication in Appendix A, 1 do not mean more background knowledge; rather I refer to the writing style. A derivation step that would usually take three or four lines to describe in the main text, would probably be done in one line in the appendix. Having said that, let me add that many of the proofs in Appendix A are, in my opinion, simpler to read than their write-ups in the original references.

The second edition of the book is organized into thirteen chapters. The first nine chapters deal with nonlinear systems analysis. Chapter 10 is also an analysis chapter, but deals with feedback systems. The last three chapter deal with the design offeedback control. Chapter 1 starts with introductory remarks on nonlinear phenomena which define the scope of the text. These remarks are followed by two sections. Section 1.1 introduces examples of nonlinear state equations which are used later in the book t o illustrate the various results and tools covered. In teaching this material, 1 have found it beneficial to get the students to appreciate the versatility of the nonlinear state equation before we overwhelm them with the technical results for that equation. Section 1.2 deals with classical material on second-order systems. I have used this material to introduce the reader to the two nonlinear phenomena which are studied rigorously later in the book; namely, multiple equilibria and their stability properties, and limit cycles.

Chapter 2 starts with a section of mathematical preliminaries. The contraction mapping theorem of Section 2.1.4 is used a few times in Appendix A, hut only once in the main text (in the proof of Theorem 2.2). If the instructor chooses to skip the proof of Theorem 2.2, then the contraction mapping theorem might be skipped. Notice, however, that normed Linear spaces, introduced in Section 2.1.4, are used in Chapter 6. Sections 2.2-2.5 contain the fundamental theory of ordinary differential , equations, which should he treated, a t least briefly without proofs.

Chapter 3 presents the Lyapunov theory. It is the core chapter of the book and should be thoroughly covered. Section 3.6 contains converse Lyapunov theorems which are referenced several times later on. It is important to mention these the- orems in the classroom. Notice, however, that both Sections 3.5 and 3.6 can he taught very briefly since their proofs can be left as reading assignments.

Beyond Chapter 3, all chapters are designed to be basically independent of each other, to give the instructor flexibility in shaping his/her course. I list here the exceptions to this general rule. The invariance theorems of Section 4.3 are used in Section 13.4 on adaptive control. Sections 5.1 t o 5.4 are used in Sections 6.2, 6.3, 6.4, 12.3, 13.1, 13.2, and 13.3, and in a few examples a t the end of Section 13.4. 1 strongly recommend coverage of Sections 5.1 to 5.4. They deal with the important topic of stability in the presence of perturbations. Despite the importance of this

Page 7: Nonlinear Systems 2nd- Hassan K. Khalil,Ch1,Ch2

vii

topic, its coverage in introductory books on Lyapunov stability has been limited, if a t all touched. To be introduced to this important aspect of Lyapunov theory, students had to consult advanced stability monographs, such as Hahn's [62] and Krasovskii's [96]. Section 5.7 on slowly varying systems is beneficial for Chapter 9 on singular perturbations and Section 11.3 on gain scheduling, but i t is not re- quired. The notion of L-stability, introduced in Section 6.1, is used in Sections 10.2 and 10.3. Familiarity with the singular perturbation theory of Chapter 9 is needed in Section 11.3, but no technical results from Chapter 9 are explicitly used. Sec- tions 11.1 and 11.2 should be included in any coverage of the last three chapters. Feedback linearizable systems, introduced in Sections 12.1 and 12.2, are used in several examples in Sections 13.1 to 13.3, but they are not needed for the main ideas of these sections.

Every chapter from 1 to 13 ends with a section of exercises which are designed to help the reader understand and apply the results and tools covered. Many of these exercises have been used in homework assignments and tests in my class over the years. A solution manual is available from the publisher.

It is my pleasure to acknowledge all those who helped me in the writing of this book. I would like, first of all, to thank my wife Amina for her encourage- ment and complete support throughout this project. I would like also to thank my sons Mohammad and Omar for their understanding and moral support. I am especially appreciative of the discussions I had with Petar KokotoviC at dif- ferent stages of this project. His remarks and suggestions were very valuable. Thanks are also due to Eyad Abed, Nazir Atassi, Martin Corless, Ahmed Dab- room, Farzad Esfandiari, Jessy Grizzle, Suhada Jayasuriya, Rolf Johansson, Ioannis Kanellakopoulos, Mustafa Khammash, P.S. Krishnaprasad, Miroslav Krstit, Zongli Lin, Semyon Meerkov, Jack Rugh, Fathi Salam, Eduardo Sontag, Mark Spong, and Steve Yurkovich, for their suggestions, constructive comments, feedback on the first edition, and/or reviewing parts of the new material of the second edition. I would like, in particular, to acknowledge Semyon Meerkov for his comprehensive feedback on the first edition and his suggestion to reorganize the book into its new form. The students in my Nonlinear Systems class a t Michigan State University have provided me with excellent feedback over the years. Finally, I would like to thank Ioannis Kanellakopoulos and Semyon Meerkov for reviewing the full second edition manuscript for Prentice Hall.

I am grateful to Michigan State IJniversity for an environment that allowed me to write this book, and to the National Science Foundation for supporting my research on singular perturbation and nonlinear feedback control; from this research endeavor I gained the experience that is necessary for writing such a book.

I am indebted to Jiansheng Hou, Sharyn Vitrano, and Elias Strangas for their help in producing the hook. Jiansheng generated all the figures of the first edition, many of which remain in the second one, Sharyn did an excellent job as the copy editor of the second edition, and Elias applied his L w expertise to help me at

Page 8: Nonlinear Systems 2nd- Hassan K. Khalil,Ch1,Ch2

3 Lyapunov Stability 3.1 Autonomous Systems . . . . . . . . . . . . . . . . . . . . . . 3.2 The lnvariance Principle . . . . . . . . . . . . . . . . . . . . . 3.3 Linear Systems and Linearization . . . . . . . . . . . . . . . .

. . . . . . . . . . . . . . . . . . . . 3.4 Nonautonomous Systems 3.5 Linear Time-Varying Systems and Linearization . . . . . . . .

. . . . . . . . . . . . . . . . . . . . . . . 3.6 Converse Theorems . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.7 Exercises

4 Advanced Stability Analysis 167 . . . . . . . . . . . . . . . . . 4.1 The Center Manifold Theorem 167

. . . . . . . . . . . . . . . . . . . . . . . 4.2 Region of Attraction 177

. . . . . . . . . . . . . . . . . . . . . . . 4.3 lnvariance Theorems 191 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.4 Exercises 196

5 Stability of Perturbed Systems 203 . . . . . . . . . . . . . . . . . . . . . 5.1 Vanishing Perturbation 204

. . . . . . . . . . . . . . . . . . . 5.2 Nonvanishing Perturbation 211 . . . . . . . . . . . . . . . . . . . . . 5.3 Input-to-State Stability 217

. . . . . . . . . . . . . . . . . . . . . . . 5.4 Comparison Method 222 . . . . . . . . . 5.5 Continuity of Solutions on the Infinite Interval 228

. . . . . . . . . . . . . . . . . . . . . 5.6 Interconnected Systems 230

. . . . . . . . . . . . . . . . . . . . . 5.7 Slowly Varying Systems 239 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.8 Exercises 250

6 Input-Output Stability 261 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.1 L Stab~l~ty 262 . . . . . . . . . . . . . . . . . . . 6.2 L Stability of State Models 269

. . . . . . . . . . . . . . . . . . . . 6.3 Input-to-Output Stability 275 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.4 L2 Gain 276 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.5 Exercises 284

7 Periodic Orbits 289 . . . . . . . . . . . . . . . . . . . . . . 7.1 Second-Order Systems 289

. . . . . . . . . . . . . . . . . . 7.2 Stability of Periodic Solutions 299 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.3 Exercises 309

8 Perturbation Theory and Averaging 313 . . . . . . . . . . . . . . . . . . . . 8.1 The Perturbation Method 314

8.2 Perturbation on the Infinite Interval . . . . . . . . . . . . . . 326 . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.3 Averaging 330

. . . . . . . . . . 8.4 Weakly Nonlinear Second-Order Oscillators 339

Page 9: Nonlinear Systems 2nd- Hassan K. Khalil,Ch1,Ch2

vii

topic, its coverage in introductory books on Lyapunov stability has been limited, if at all touched. To be introduced to this important aspect of Lyapunov theory, students had to consult advanced stability monographs, such as Bahn's [62] and Krasovskii's [96]. Section 5.7 on slowly varying systems is beneficial for Chapter 9 on singular perturbations and Section 11.3 on gain scheduling, hut it is not re- quired. The notion of L-stability, introduced in Section 6.1, is used in Sections 10.2 and 10.3. Familiarity with the singular perturbation theory of Chapter 9 is needed in Section 11.3, but no technical results from Chapter 9 are explicitly used. Sec- tions 11.1 and 11.2 should be included in any coverage of the last three chapters. Feedback linearizable systems, introduced in Sections 12.1 and 12.2, are used in several examples in Sections 13.1 to 13.3, but they are not needed for the main ideas of these sections.

Every chapter from 1 to 13 ends with a section of exercises which are designed to help the reader understand and apply the results and tools covered. Many of these exercises have been used in homework assignments and tests in my class over the years. A solution manual is available from the publisher.

It is my pleasure to acknowledge all those who helped me in the writing of this book. I would like, first of all, to thank my wife Amina for her encourage- ment and complete support throughout this project. I would like also to thank my sons Mohammad and Omar for their understanding and moral support. I am especially appreciative of the discussions I had with Petar KokotoviE at dif- ferent stages of this project. His remarks and suggestions were very valuable. Thanks are also due to Eyad Abed, Nazir Atassi, Martin Corless, Ahmed Dah- room, Farzad Esfandiari, Jessy Grizzle, Suhada Jayasuriya, Rolf Johansson, Ioannis Kanellakopoulos, Mustafa Khammash, P.S. Krishnaprasad, Miroslav KrstiC, Zongli Lin, Semyon Meerkov, Jack Rugh, Fathi Salam, Eduardo Sontag, Mark Spong, and Steve Yurkovich, for their suggestions, constructive comments, feedback on the first edition, and/or reviewing parts of the new material of the second edition. I would like, in particular, to acknowledge Semyon Meerkov for his comprehensive feedback on the first edition and his suggestion to reorganize the book into its new form. The students in my Nonlinear Systems class at Michigan State University have provided me with excellent feedback over the years. Finally, I would like to thank Ioannis Kanellakopoulos and Semyon Meerkov for reviewing the full second edition manuscript for Prentice Hall.

I am grateful to Michigan State liniversity for an environment that allowed me to write this hook, and to the National Science Foundation for supporting my research on singular perturbation and nonlinear feedback control; from this research endeavor I gained the experience that is necessary for writing such a book.

I am indebted to Jiansheng Hou, Sharyn Vitrano, and Elias Strangas for their help in producing the hook. Jiansheng generated all the figures of the first edition, many of which remain in the second one, Sharyn did an excellent job as the copy editor of the second edition, and Elias applied his SQX expertise to help me at

Page 10: Nonlinear Systems 2nd- Hassan K. Khalil,Ch1,Ch2

viii

critical times. The hook was typeset using All computations, including numerical solu-

tion of differential equations, were done using MATLAB. The figures were generated using FrameMaker, MATLAB, or the graphics tool of L w .

Hassan Khalil East Lansing, Michigan

Page 11: Nonlinear Systems 2nd- Hassan K. Khalil,Ch1,Ch2

Contents

1 Introduction 1 1.1 Examples . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5

. . . . . . . . . . . . . . . . . . . 1.1.1 Pendulum Equation 5 . . . . . . . . . . . . . . . . . . 1.1.2 Tunnel Diode Circuit 7

. . . . . . . . . . . . . . . . . . . 1.1.3 Mass-Spring System 8 . . . . . . . . . . . . . 1.1.4 Negative-Resistance Oscillator 11

. . . . . . . . . . . . . . . . 1.1.5 Artificial Neural Network 14 . . . . . . . . . . . . . . . . . . . . 1.1.6 Adaptive Control 16

. . . . . . . . . . . . . . . . . . . . . . 1.2 Second-Order Systems 19 . . . . . . . . . 1.2.1 Qualitative Behavior of Linear Systems 23

. . . . . . . . . . . . . . . . . . . . 1.2.2 Multiple Equilibria 33 . . . . . 1.2.3 Qualitative Behavior Near Equilibrium Points 36

. . . . . . . . . . . . . . . . . . . . . . . 1.2.4 Limit Cycles 41 . . . . . . . 1.2.5 Numerical Construction o f Phase Portraits 46

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.3 Exercises 47

2 Fundamental Properties 57 . . . . . . . . . . . . . . . . . . . 2.1 Mathematical Preliminaries 58

2.1.1 Euclidean Space . . . . . . . . . . . . . . . . . . . . . 58 2.1.2 Mean Value and Implicit Function Theorems . . . . . . 62

. . . . . . . . . . . . . . 2.1.3 Gronwall-Bellman Inequality 63 . . . . . . . . . . . . . . . . . . 2.1.4 Contraction Mapping 64

. . . . . . . . . . . . . . . . . . . . 2.2 Existence and Uniqueness 67 2.3 Continuous Dependence on Initial Conditions

. . . . . . . . . . . . . . . . . . . . . . . . . and Parameters 78 2.4 Differentiability of Solutions and Sensitivity

. . . . . . . . . . . . . . . . . . . . . . . . . . . . Equations 81 . . . . . . . . . . . . . . . . . . . . . . 2.5 Comparison Principle 84

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.6 Exercises 88

Page 12: Nonlinear Systems 2nd- Hassan K. Khalil,Ch1,Ch2

3 Lyapunov Stability 3.1 Autonomous Systems . . . . . . . . . . . . . . . . . . . . . . 3.2 The lnvariance Principle . . . . . . . . . . . . . . . . . . . . . 3.3 Linear Systems and Linearization . . . . . . . . . . . . . . . . 3.4 Nonautonomous Systems . . . . . . . . . . . . . . . . . . . . 3.5 Linear Time-Varying Systems and Linearization . . . . . . . . 3.6 Converse Theorems . . . . . . . . . . . . . . . . . . . . . . .

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.7 Exercises

4 Advanced Stabil i ty Analysis 4.1 The Center Manifold Theorem . . . . . . . . . . . . . . . . . 4.2 Region o f Attraction . . . . . . . . . . . . . . . . . . . . . . .

. . . . . . . . . . . . . . . . . . . . . . . 4.3 lnvariance Theorems 4.4 Exercises . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

5 Stabil i ty of Perturbed Systems 203 5.1 Vanishing Perturbation . . . . . . . . . . . . . . . . . . . . . 204 5.2 Nonvanishing Perturbation . . . . . . . . . . . . . . . . . . . 211 5.3 Input-to-State Stability . . . . . . . . . . . . . . . . . . . . . 217 5.4 Comparison Method . . . . . . . . . . . . . . . . . . . . . . . 222

. . . . . . . . . 5.5 Continuity of Solutions on the Infinite Interval 228 5.6 Interconnected Systems . . . . . . . . . . . . . . . . . . . . . 230 5.7 Slowly Varying Systems . . . . . . . . . . . . . . . . . . . . . 239 5.8 Exercises . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 250

6 Input-Output Stability 26 1 6.1 LStabi l i ty . . . . . . . . . . . . . . . . . . . . . . . . . . . . 262 6.2 L Stability o f State Models . . . . . . . . . . . . . . . . . . . 269 6.3 Input-to-Output Stability . . . . . . . . . . . . . . . . . . . . 275 6.4 L z Gain . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 276 6.5 Exercises . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 284

7 Periodic Orbits 289 7.1 Second-Order Systems . . . . . . . . . . . . . . . . . . . . . . 289 7.2 Stability of Periodic Solutions . . . . . . . . . . . . . . . . . . 299 7.3 Exercises . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 309

8 Perturbation Theory and Averaging 313 8.1 The Perturbation Method . . . . . . . . . . . . . . . . . . . . 314 8.2 Perturbation on the Infinite Interval . . . . . . . . . . . . . . 326 8.3 Averaging . . . . . . . . . . . . . . . . . . . . . . . . . . . . 330 8.4 Weakly Nonlinear Second-Order Oscillators . . . . . . . . . . 339

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. . . . . . . . . . . . . . . . . . . . . . . . 8.5 General Averaging 342 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.6 Exercises 347

9 Singular Perturbat ions 351 . . . . . . . . . . . 9.1 The Standard Singular Perturbation Model 352

. . . . . . . . . 9.2 Time-Scale Properties of the Standard Model 358 . . . . . . . . . . . . . . . . . . . . 9.3 Slow and Fast Manifolds 365

. . . . . . . . . . . . . . . . . . . . . . . . 9.4 Stability Analysis 372 . . . . . . . . . . 9.5 Singular Perturbation on the Infinite Interval 384

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.6 Exercises 388

10 Analysis o f Feedback Systems . . . . . . . . . . . . . 10.1 Absolute Stability

10.1.1 Circle Criterion . . . . . . . . . . 10.1.2 Popov Criterion . . . . . . . . . . 10.1.3 Simultaneous Lyapunov Functions

10.2 Srnall-Gain Theorem . . . . . . . . . . . . . . . . . . . . . . . . 10.3 Passivity Approach

10.4 The Describing Function Method . . . . . 10.5 Exercises . . . . . . . . . . . . . . . . . .

11 Feedback Con t ro l 479 . . . . . . . . . . . . . . . . . . . . . . . . 11.1 Control Problems 479

. . . . . . . . . . . . . . . . . . . . . 11.2 Design via Linearization 485 . . . . . . . . . . . . . . . . . . . . . . 11.2.1 Stabi l izat ion 485

. . . . . . . . . . . . 11.2.2 Regulat ion v i a In tegra l Cont ro l 488 . . . . . . . . . . . . . . . . . . . . . . . . . 11.3 Gain Scheduling 493

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11.4 Exercises 509

12 Exac t Feedback L inear izat ion . . . . . . . . . . . . . . . . . . . . 12.1 lnput-State Linearization

. . . . . . . . . . . . . . . . . . . 12.2 lnput-Output Linearization 12.3 State Feedback Control . . . . . . . . . . . . . . . . . . . . .

. . . . . . . . . . . . . . . . . . . . . . 12.3.1 Stabi l izat ion 12.3.2 Track ing . . . . . . . . . . . . . . . . . . . . . . . . . 12.3.3 Regulat ion v i a In tegra l Cont ro l . . . . . . . . . . . .

12.4 Differential Geometric Approach . . . . . . . . . . . . . . . . 12.4.1 Differential Geometr ic Tools . . . . . . . . . . . . . .

. . . . . . . . . . . . . . 12.4.2 I npu t -Ou tpu t L inear izat ion . . . . . . . . . . . . . . . 12.4.3 Input-State L inear izat ion

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12.5 Exercises

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13 Lyapunov-Based Design 577 13.1 Lyapunov Redesign . . . . . . . . . . . . . . . . . . . . . . . 578

13.1.1 Robust Stabilization . . . . . . . . . . . . . . . . . . . 578 13.1.2 Nonlinear Damping . . . . . . . . . . . . . . . . . . 586

13.2 Backstepping . . . . . . . . . . . . . . . . . . . . . . . . . 588 13.3 Sliding Mode Control . . . . . . . . . . . . . . . . . . . . . . 601 13.4 Adaptive Control . . . . . . . . . . . . . . . . . . . . . . . . 617

13.4.1 Model Reference Controller . . . . . . . . . . . . . . 618 . . . . . . . . . . 13.4.2 Model Reference Adaptive Control 622

13.5 Exercises . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 640

Appendix A 651 A . l Proof of Lemma 2.5 . . . . . . . . . . . . . . . . . . . . . . . 651 A.2 Proof of Lemma 3.1 . . . . . . . . . . . . . . . . . . . . . . . 652 A.3 Proof of Lemma 3.3 . . . . . . . . . . . . . . . . . . . . . . . 653 A.4 Proof of Lemma 3.4 . . . . . . . . . . . . . . . . . . . . . . . 656 A.5 Proof of Lemma 3.5 . . . . . . . . . . . . . . . . . . . . . . . 657 A.6 Proof of Theorem 3.14 . . . . . . . . . . . . . . . . . . . . . 657 A.7 Proof of Theorems 4.1 and 4.3 . . . . . . . . . . . . . . . . . 661 A.8 Proof of Lemma 4.1 . . . . . . . . . . . . . . . . . . . . . . . 668 A.9 Proof o f Theorem 6.4 . . . . . . . . . . . . . . . . . . . . . . 669 A.10 Proof of Theorem 7.1 . . . . . . . . . . . . . . . . . . . . . . 671 A.11 Proof of Theorem 8.2 . . . . . . . . . . . . . . . . . . . . . . 674 A.12 Proof of Theorem 8.3 . . . . . . . . . . . . . . . . . . . . . . 676 A.13 Proof of Theorem 8.4 . . . . . . . . . . . . . . . . . . . . . . 680 A.14 Proof of Theorem 9.1 . . . . . . . . . . . . . . . . . . . . . . 681 A.15 Proof of Thvorem 9.4 . . . . . . . . . . . . . . . . . . . . . . 686 A.16 Proof o f Lemma 10.1 . . . . . . . . . . . . . . . . . . . . . . 688 A.17 Proof of Lemma 10.2 . . . . . . . . . . . . . . . . . . . . . . 691 A.18 Proof of Lemma 10.7 . . . . . . . . . . . . . . . . . . . . . . 694 A.19 Proof o f Theorem 10.9 . . . . . . . . . . . . . . . . . . . . . 698 A.20 Proof of Lemma 13.4 . . . . . . . . . . . . . . . . . . . . . . 701 A.21 Proof o f Lemma 13.5 . . . . . . . . . . . . . . . . . . . . . . 704

Notes and References

Bibliography

Symbols

Index

Page 15: Nonlinear Systems 2nd- Hassan K. Khalil,Ch1,Ch2

Chapter 1

Introduction

When engineers analyze and design nonlinear dynamical systems in electrical cir- cuits, mechanical systems, control systems, and other engineering disciplines, they need to absorb and digest a wide range of nonlinear analysis tools. In this book, we introduce some of the these tools. In particular, we present tools for stability analy- sis of nonlinear systems, with an emphasis on Lyapunov's method. We give special attention to the stability of feedback systems. We present tools for the detection and analysis of "free" oscillations, including the describing function method. We introduce the asymptotic tools of perturbation theory, including averaging and sin- gular perturbations. Finally, we introduce nonlinear feedback control tools, includ- ing linearization, gain scheduling, exact feedback linearization, Lyapunov redesign, backstepping, sliding mode control, and adaptive control.

We shall deal with dynamical systems which are modeled by a finite number of coupled first-order ordinary differential equations

where xi denotes the derivative of z, with respect to the time variable t , and UI, u2, . . ., up are specified input variables. We call the variables zl, 22, . . ., z, the state variables. They represent the memory that the dynamical system bas of its past. We usually use vector notation to write the above equations in a compact

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2 CHAPTER 1 INTRODUCTIOh

form Define

and rewrite the n first-order differential equations as one n-dimensional first-order vector differential equation

x = f ( t , z , u ) (1.1)

We call (1.1) the state equation, and refer to x as the state and u as the input. Sometimes, we associate with (1.1) another equation

y = h ( t , x , u ) (1.2)

which defines a q-dimensional output vector that comprises variables of particular interest in the analysis of the dynamical system, like variables which can be phys- ically measured or variables which are required to behave in a specified manner. We call (1.2) the output equation and refer to equations (1.1) and (1.2) together as the state-space model, or simply the state model. Mathematical models of finite- dimensional physical systems do not always come in the form of a state-space model. However, more often than not, we can model physical systems in this form by care- fully choosing the state variables. Examples and exercises that will appear later in this chapter will demonstrate the versatility of the state-space model.

Most of our analysis in this book will deal with the state equation, and many times without explicit presence of an input u , that is, the so-called unforced state equation

x = f ( t , x ) ( ' 3 )

Working with an unforced state equation does not necessarily mean that the input to the system is zero. It could be that the input has been specified as a given , function of time, u = y(t), a given feedback function of the state, u = y(x), or both, u = y(t, 2). Substitution of u = y in (1.1) eliminates u and yields an unforced state equation.

A special case of (1.3) arises when the function f does not depend explicitly on 1; that is,

x = f (x) (1.4)

Page 17: Nonlinear Systems 2nd- Hassan K. Khalil,Ch1,Ch2

in which case the system is said to be aulonomovs or time invariant. The behavior of an autonomons system is invariant to shifts in the time origin, since changing the time variable from t to r = t - a does not change the right-hand side of the state equation. If the system is not autonomous, then it is called nonavtonomous or lime varying.

An important concept in dealing with the state equation is the concept of an equilibrium point. A point s = z* in the state space is said to be an equilibrium point of (1.3) if i t has the property that whenever the state of the system starts a t x* it will remain a t x* for all future time. For the autonomous system (1.4), the equilibrium points are the real roots of the equation

f(x) = 0

A4 equilibrium point could be isolated; that is, there are no other equilibrium points in its vicinity, or there could be a continuum of equilibrium points.

For linear systems, the state-space model (1.1)-(1.2) takes the special form

x = A(t)x + B(t)u y = C(t)x + D(t)u

We assume that the reader is familiar with the powerful analysis tools for linear systems, founded on the basis of the superposition principle. As we move from linear to nonlinear systems, we are faced with a more difficult situation. The superposi- tion principle does not hold any longer, and analysis tools involve more advanced mathematics. Because of the powerful tools we know for linear systems, the first step in analyzing a nonlinear syst,em is usually to linearize i t , if possible, about some nominal operating point and analyze the resulting linear model. This is a common practice in engineering, and it is a useful one. There is no question that, whenever possible, we should make use of linearization to learn as much as we can about the behavior of a nonlinear system. However, linearization alone will not be sufficient; we must develop tools for the analysis of nonlinear systems. There are two basic limitations of linearization. First, since linearization is an approxi- mation in the neighborhood of an operating point, i t can only predict the "local" behavior of the nonlinear system in the vicinity of that point. I t cannot predict the "nonlocal" behavior far from the operating point, and certainly not the "global" behavior throughout the state space. Second, the dynamics of a nonlinear system are much richer than the dynamics of a linear system. There are 'Lessentially non- linear phenomena" that can take place only in the presence of nonlinearity; hence, they cannot be described or predicred by linear models. Examples of essentially nonlinear phenomena are: . Finite escape lime: The state of an unstable linear system goes to infinity

as time approaches infinity; a nonlinear system's state, however, can go to infinity in finite time.

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4 CHAPTER 1. INTRODUCTION

Multiple isolated equilibria: A linear system can have only one isolated equi- librium point; hence, it can have only one steady-state operating point which attracts the state of the system irrespective of the initial state. A nonlinear system can have more than one isolated equilibrium point. The state may converge to one of several steady-state operating points, depending on the initial state of the system.

Limit cycles: For a linear time-invariant system to oscillate, it must have a pair of eigenvalues on the imaginary axis, which is a nonrobust condition that is almost impossible t o maintain in the presence of perturbations. Even if we do, the amplitude of oscillation will be dependent on the initial state. In real life, stable oscillation must be produced by nonlinear systems. There are nonlinear systems which can go into an oscillation of fixed amplitude and frequency, irrespective of the initial state. This type of oscillation is known as a limit cycle.

Subharmonic, harmonic, o r almost-periodic oscillations: A stahle linear sys- tem under a periodic input produces an output of the same frequency. A non- linear system under periodic excitation can oscillate with frequencies which are submultiples or multiples of the input frequency. It may even generate an almost-periodic oscillation, an example of which is the sum of periodic oscillations with frequencies which are not multiples of each other.

Chaos: A nonlinear system can have a more complicated steady-state behavior that is not equilibrium, periodic oscillation, or almost-periodic oscillation. Such behavior is usually referred to as chaos. Some of these chaotic motions exhibit randomness, despite the deterministic nature of the system.

Multiple modes of behavior: It is not unusual for two or more modes of b e havior t o be exhibited by the same nonlinear system. An unforced system may have more than one limit cycle. A forced system with periodic excita- tion may exhibit harmonic, subharmonic, or more complicated steady-state behavior, depending upon the amplitude and frequency of the input. It may even exhibit a discontinuous jump in the mode of behavior as the amplitude or frequency of the excitation is smoothly changed.

In this book, we shall encounter only the first three of these phenomena.' Multiple equilibria and limit cycles will be introduced later in this chapter, as we examine second-order autonomous systems, while the phenomenon of finite escape time will be introduced in Chapter 2.

'To read about forced oscillation, chaos, bifurcation, and other important topics, the reader may consult [59], [64]. and [183].

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1 .l. EXAMPLES 5

Figure 1.1: Pendulum.

1.1 Examples

1.1.1 Pendulum Equation

Consider the simple pendulum shown in Figure 1.1, where I denotes the length of the rod and m denotes the mass of the hob. Assume the rod is rigid and has zero mass. Let B denote the angle suhtended by the rod and the vertical axis through the pivot point. The pendulum is free to swing in the vertical plane. The bob of the pendulum moves in a circle of radius I. To write the equation of motion of the pendulum, let us identify the forces acting on the bob. There is a downward gravitational force equal to mg, where g is the acceleration due to gravity. There is also a frictional force resisting the motion, which we assume to he proportional to the speed of the bob with a coefficient of friction k. Using Newton's second law of motion, we can write the equation of motion in the tangential direction as

mlB = -mg sin 8 - kle Writing the equation of motion in the tangential direction has the advantage that the rod tension, which is in the normal direction, does not appear in the equation. Note that we could have arrived at the same equation by writing the moment equation about the pivot point. To obtain a state-space model of the pendulum, let us take the state variables as zl = 8 and xz = 8. Then, the state equation is

To find the equilibrium points, we set x, = zz = 0 and solve for xi and 22

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6 CHAPTER 1. INTRODUCTION

The equilibrium points are located at (nx, 0), for n = 0, *l, k2,. . .. From the phys- ical description of the pendulum, it is clear that the pendulum has only two equi- librium positions corresponding to the equilibrium points (0,0) and (x,O). Other equilibrium points are repetitions of these two positions which correspond to the number of full swings the pendulum would make before it rests a t one of the two equilibrium positions. For example, if the pendulum makes m complete 360' revolu- tions before it rests a t the downward vertical position, then mathematically we say that the pendulum approaches the equilibrium point (2mrr, 0). In our investigation of the pendulum, we will limit our attention to the two "nontrivial" equilibrium points a t (0,0) and (rr, 0). Physically, we can see that these two equilibrium posi- tions are quite distinct from each other. While the pendulum can indeed rest a t the (0,O) equilibrium point, i t can hardly maintain rest a t the (n, 0) equilibrium point because infinitesimally small disturbance from that equilibrium will take the pen- dulum away. The difference between the two equilibrium points is in their stability properties, a topic we shall study in some depth.

Sometimes it is instructive to consider a version of the pendulum equation where the frictional resistance is neglected by setting k = 0. The resulting equation

is conservative in the sense that if the pendulum is given an initial push, i t will keep oscillating forever with a nondissipative energy exchange between kinetic and potential energies. This, of course, is not realistic but gives insight into the behavior of the pendulum. It may also help in finding approximate solutions of the pendulum equation when the friction coefficient k is small. Another version of the pendulum equation arises if we can apply a torque T to the pendulum. This torque may he viewed as a control input in t,he equation

Interestingly enough, several unrelated physical systems are modeled by equations similar to the pendulum equation. Such examples are the model of a synchronous generator connerted to an infinite bus (Exercise 1.7), the model of a Josephson junction circuit (Exercise 1.8), and the model of a phase-locked loop (Exercise 1.10). Consequently, the pendulum equation is of great practical importance.

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1 . I . EXAMPLES 7

Figure 1.2: (a) Tunnel diode circuit; ( b ) Tunnel diode U R - i R characteristic.

1.1.2 Tunnel Diode Circuit

Consider the tunnel diode circuit shown in Figure 1.2,2 where the tunnel diode is characterized by iR = h ( v ~ ) . The energy-storing elements in this circuit are the capacitor C and the inductor L. Assuming they are linear and time-invariant, we can model them by the equations

where i and u are the current through and the voltage across an element, with the subscript specifying the element. To write a state-space model for the system, let us take zl = v c and x2 = iL as the state variables, and u = E as a constant input. To write the state equation for zl, we need to express ic as a function of the state variables zl,zz and the input u. Using Kirchhoff's current law, we can write an equation that the algebraic sum of all currents leaving node @ is equal to zero:

Hence, ic = -h(z~) + 2 2

Similarly, we need to express 0,. as a function of the state variables zl, z2 and the input u. Using Kirchhoff's voltage law, we can write an equation that the algebraic sum of all voltages across elements in the left loop is equal to zero:

2This figure, as well as Figures 1.3 and 1.6, are taken from [33]

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8 CHAPTER 1. INTRODUCTION

Hence, v,, = -I I - R x z + u

We can now write the state-space model for the circuit as

1 X I = -d [ - h ( ~ ~ ) + x z l (1.11)

The equilihrium points of the system are determined by setting X I = x2 = 0 and solving for XI and xz

Therefore, the equilibrium points correspond to the roots of the equation

Figure 1.3 shows graphically that for certain values of E and R this equation has three isolated roots which correspond to three isolated equilibrium points of the system. The number of equilibrium points might change as the values of E and R change. For example, if we increase E for the same value of R we will reach a point beyond which only the point QJ will exist. On the other hand, if we decrease E for the same value of R, we will end up with the point QI as the only equilibrium. Suppose we are in the multiple equilibria situation: Which of these equilibrium points can we observe in an experimental setup of this circuit? The answer depends on the stability properties of the equilibrium points. We will come back to this example later in the chapter and answer this question.

1.1.3 Mass-Spring System

In the mass-spring mechanical system, shown in Figure 1.4, we consider a mass m sliding on a horizontal surface and attached to a vertical surface through a spring. The mass is subjected to an external force F . We define y as the displacement from a reference position and write Newton's law of motion

where Ff is a resistive force due t o friction and F,p is the restoring force of the spring. We assume that Fap is a function only of the displacement y and write it as Fap = s(Y). We assume also that the reference position has been chosen such that

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1.1. EXAMPLES 9

Figure 1.3: Equilibrium points of the tunnel diode circuit.

Figure 1.4: Mass-spring mechanical system

g ( 0 ) = 0. The external force F is at our disposal. Depending upon F, Ft, and g, several interesting autonomous and nonautonomous second-order models arise.

For a relatively small displacement, the restoring force of the spring can be modeled as a linear function g ( y ) = k y , where k is the spring constant. For a large displacement, however, the restoring force may depend nonlinearly on y. For example, the function

models the so-called softening spring where, beyond a certain displacement, a large displacement increment produces a small force increment. On the other hand, the function

S ( Y ) = k ( l + a 2 y 2 ) y

models the so-called hardening spring where, beyond a certain displacement, a small displacement increment produces a large force increment.

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10 CHAPTER 1. INTRODUCTION

As the mass moves in the air (a viscous medium) there will be a frictional force due to viscosity. This force is usually modeled as a nonlinear function of the velocity; that is, F, = h(y) where h(0) = 0. For small velocity, we can assume that E", = cy. The combination of a hardening spring, linear viscous damping, and a FIeriodic external force F = A coswt results in the Duffing's equation

my + cy + ky + kaZy3 = Acoswt (1.13)

which is a classical example in the study of periodic excitation of nonlinear systems. As another exampleof a frictional force, we consider the so-called dry or Coulomb

friction. This type of damping arises when the mass slides on a dry surface. When the mass is at rest, there is a static friction force F, that acts parallel to the surface and is limited to fp ,mg, where 0 < p, < 1 is the static friction coefficient. This force takes whatever value, between its limits, to keep the mass at rest. For motion to begin, there must be a force acting on the mass to overcome the resistance to motion caused by static friction. In the absence of an external force, F = 0, the static friction force will balance the restoring force of the spring and maintain equilibrium for lg(y)l < p,mg. Once motion has started, there is a slipping friction force of magnitudepkmg that resists the motion of the mass, where PI. is the kinetic friction coefficient, which we assume to be constant. As an idealization of the dry friction force, we may define it as

-ptmg, for y < 0 f i = { , for i = o

ptmg, for y > O

The combination of a linear spring, linear viscous damping, dry friction, and zero external force results in

where

ptmg sign(y), for 1y1 > 0 for y = O and lyl <p,mg/k

-p,mg sign(y), for y = 0 and lyl > p,mg/k

The value of ~ ( y , y) for y = 0 and lyl < p.mg/k is obtained from the equilibrium condition y = y = 0. With zl = y and 2 2 = i , the state equation is

Let us note two features of this state equation. First, it has an equilibrium set rather than isolated equilibrium points. Second, the right-hand side function is

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1.1. EXAMPLES 11

a discontinuous function of the state. The discontinuity is a consequence of the idealization we adopted in modeling the dry friction. One would expect the physical dry friction to change from its static friction mode into its slipping friction mode in a smooth way, not abruptly as our idealization suggests. The advantage of the discontinuous idealization is that i t allows us to simplify the analysis. For example, when xz > 0, we can model the system by the linear model

Similarly, when xz < 0, we can model i t by the linear model

Thus, in each region we can predict the behavior of the system via linear analysis. This is an example of the so-called piecewise linear analysis, where a system is represented by linear models in various regions of the state space, certain coefficients changing from region to region.

1.1.4 Negative-Resistance Oscillator

Figure 1.5 shows the basic circuit structure of an important class of electronic oscillators. The inductor and capacitor are assumed to he linear, timeinvariant and passive, that is, L > 0 and C > 0. The resistive element is an active circuit characterized by the voltage-controlled i - v characteristic i = h(u), shown in the figure. The function h(.) satisfies the conditions

h(v) + w as v --r cu, and h(v) + -ce as u -r -a

where hf(v) is the first derivative of h(v) with respect to u. Such i-v characteristic can he realized, for example, by the twin-tunnel-diode circuit of Figure 1.6. Using Kirchhoff's current law, we can write the equation

Hence

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12 CHAPTER 1. INTRODUCTION

Resistive

Element

(a) (b)

Figure 1.5: (a) Basic oscillator circuit; (b) Typical nonlinear driving-point characteris- tic.

Figure 1.6: A negativeresistance twin-tunnel-diode circuit.

Differentiating once with respect to t and multiplying through by L, we obtain

d2v dv C L - + v + Lhl(u)- = 0

dt2 dt

This equation can be written in a form that coincides with some well-known equa- tions in nonlinear systems theory. To do that, let us change the time variable from t to T = t/m. The derivatives of v with respect to t and r are related by

dv - - d7

- ad" dt

dav - - d2u dr2

- C L - dt2

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1.1. EXAMPLES 13

Denoting the derivative of v with respect to T by w, we can rewrite the circuit equation as

v + rh1(v)6 + v = 0

where E = m. This equation is a special case of Liinard's equation

When h ( v ) = -v + i v 3

the circuit equation takes the form

which is known as the Van der Pol equation. This equation, which was used by Van der Pol to study oscillations in vacuum tube circuits, is a fundamental example in nonlinear oscillation theory. It possesses a periodic solution that attracts every other solution except the trivial one at the unique equilibrium point v = v = 0. To write a state-space model for the circuit, let us take xl = v and x2 = 6 to obtain

21 = zz (1.18)

22 = - X I - ~ h ' ( z i ) x ~ (1 .19)

Note that an alternate state-space model could have been obtained by choosing the state variables as the voltage across the capacitor and the current through the inductor, as we did in the previous example. Denoting the state variables by zl = ir. and zz = v c , the state-space model is given by

Since the first state-space model has been written with respect to the time variable r = t/m, let us write this model with respect to T.

The state-space models in z and z look different, but they are equivalent represen- tations of the system. This equivalence can be seen by noting that these models can be obtained from each other by a change of coordinates

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14 CHAPTER 1. INTRODUCTION

Conductor

Inverting Ampifier

Amplifier

Conductor I

Invertine Am~ifier - &

Amplifier

Figure 1.7: Hopfield neural network model

Since we have chosen both 2: and z in terms of the physical variables of the circuit, it is not hard to find the map T ( . ) . We have

Thus,

and the inverse mapping is

1.1.5 Artificial Neural Network

Artificial neural networks, in analogy to biological structures, take advantage of distributed information processing and their inherent potential for parallel compu- tation. Figure 1.7 shows an electric circuit that implements one model of neural networks, known as the Hopjield model . The circuit is based on an RC network connecting amplifiers. The input-output characteristics of the amplifiers are given by li; = gi(ui), where ui and I/; are the input and output voltages of the ith am- plifier. The function g i ( . ) : R + ( -VM, VM) is a sigmoid function with asymptotes -VM and VM, as shown in Figure 1.8 for a case with VM = 1. It is continuously differentiable, odd, monotonically increasing, and gi(ui) = 0 if and only if ui = 0.

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1.1. EXAMPLES 15

Figure 1.8: A typical input-output characteristic for the amplifiers in Hopfield network.

Examples of possible g,(.) are

and

where X is the slope of gi(ui) at ui = 0. Such sigmoid input-output characteristics can be realized using operational amplifiers. For each amplifier, the circuit contains an inverting amplifier whose output is -V,, which permits a choice of the sign of the amplifier output that is connected to a given input line. The outputs V, and -K are usually provided by two output terminals of the same operational amplifier circuit. ?'he pair of nonlinear amplifiers is referred to as a "neuron." The circuit also contains an RC section a t the input of each amplifier. The capacitance C; > 0 and the resistance pi > 0 represent the total shunt capacitance and shunt resistance at the ith amplifier input. Writing Kirchhoff's current law at the input node of the ith amplifier, we obtain

where

Rij is the resistor connecting the output of the j th amplifier to the ith input line, zj is a signed conductance whose magnitude is l/Rij and whose sign is determined by the choice of the positive or negative output of the j th amplifier, and Ii represent any other constant input current (not shown in the figure). For a circuit containing n amplifiers, the motion is described by n first-order differential equations. To write a state-space model for the circuit, let us choose the state variables as zi = V, for

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16 CHAPTER 1. INTRODUCTION

i = 1 , 2 , . . ., n. Then

du;

Defining

we can write the state equation as

for i = 1 , 2 , . . . , n. Note that, due to the sigmoid characteristic of gi(.), the function hi(.) satisfies

hi(zi) > 0, V xi E (-VM,VM)

The equilibrium points of the system are the roots of the n simultaneous equations

They are determined by the sigmoid characteristics, the linear resistive connection, and the input currents. We can obtain an equivalent statespace model by choosing the state variables as the voltage at the amplifier inputs ui.

Stability analysis of this neural network depends critically on whether the sym- metry condition Ej = Tji is satisfied. An example of the analysis when Ti, = Tji is given in Section 3.2, while an example when Til # q; is given in Section 5.6.

1.1.6 Adaptive Control

Consider a first-order linear system described by the model

Gp = a p y p + kpu where u is the control input and yp is the measured output. We shall refer to thls system as the plant. Suppose i t is desirable to obtain a closed-loop system whose input-output behavior is described by the reference model

~m = amym + k m ~

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1.1. EXAMPLES 17

where r is the reference input and the model has been chosen such that y,( t ) represents the desired output of the closed-loop system. This goal can be achieved by the linear feedback control

provided that the plant parameters a p and k p are known, kp # 0, and the controller parameters 0: and 0; are chosen as

When a p and k, are unknown, we may consider the controller

where the time-varying gains 6'1(t) and Oz(t) are adjusted on-line using the available data, namely, T ( T ) , Y , (T) , y p ( r ) , and u(r) for T < t . The adaptation should be such that Bl( t ) and Oz( t ) evolve to their nominal values 8; and 8 ; . The adaptation rule is chosen based on stability considerations. One such rule, known as the gradient algorithm: is to use

where y is a positive constant that determines the speed of adaptation. This adap- tive control law assumes that the sign of k, is known and, without loss of generality, takes it to be positive. To write a state-space model that describes the closed-loop system under the adaptive control law, it is more convenient to define the output error e , and the parameter errors 41 and 4 2 as

Using the definition of 0 ; and b'i, the reference model can be rewritten as

On the other hand, the plant output yp satisfies the equation

Subtracting the above two equations, we obtain the error equation

= a p e , + k,(01 - B;)r + k p ( 8 2 ~ p - 6 ' ; ~ ~ )

= apeo + kp(B1 - 0 ; ) ~ + kp(02yp - B;ym + 6;yp - 0 ; ~ ~ ) = ( a p + kp6';)eo + kP(B1 - 8 ; ) ~ + kp(02 - B;)yp

3This adaptation rule will be derived in Section 13.4.

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18 CHAPTER 1. INTRODUCTION

Thus, the closed-loop system is described by the nonlinear, nonautonomous, third- order state equation

where we have used $ , ( t ) = 8 , ( t ) and wrote r ( t ) and y,(t) as explicit functions of time to emphasize the nonautonomous nature of the system. The signals r ( t ) and ym( t ) are the external driving inputs of the dosed-loop system.

A simpler version of this model arises if we know k p . In this case, we can take 81 = 8; and only 82 needs to be adjusted on-line. The closed-loop model reduces to

where we have dropped the subscript from 4 2 . If the goal of the control design is to regulate the plant output yp to zero, we take r ( t ) = 0 (hence, ym(t ) r 0) and the closed-loop model simplifies to the autonomous second-order model

60 = ( a , + kp4)e ,

4 = -ye:

The equilibrium points of this system are determined by setting i, = $ = 0 to obtain the algebraic equations

The system has equilibrium at e , = 0 for all values of 4 ; that is, it has an equilibrium set e, = 0. There are no isolated equilibrium points.

The particular adaptive control scheme described here is called direct model reference adaptive control. The term "model reference" stems from the fact that the controller's task is to match a given closed-loop reference model, while the term "direct" is used to indicate that the controller parameters are adapted di- rectly as opposed, for example, to an adaptive control scheme that would estimate the plant parameters ap and kp on line and use their estimates to calculate the controller parameters. We shall not describe the various possible adaptive control ~ c h e m e s . ~ However, the analysis of direct model reference adaptive control that we shall present is typical for other adaptive controls. The adaptive control problem

'For a comprehensive treatment of adaptive control, the reader may consult [4], [ I l l , [79], [122], or [151].

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1.2. SECOND-ORDER SYSTEMS 19

will generate some interesting nonlinear models like the second- and third-order models we have just derived, which will he used to illustrate some of the stability and perturbation techniques of this book. A more general description of model reference adaptive control and its stability analysis will he pursued in Section 13.4.

1.2 Second-Order Systems

Second-order autonomous systems occupy an important place in the study of non- linear systems because solution trajectories can be represented by curves in the plane. This allows easy visualization of the qualitative behavior of the system. The purpose of this section is t o use second-order systems to introduce, in an elementary context, some of the basic ideas of nonlinear systems. In particular, we shall look a t the behavior of a nonlinear system near equilibrium points and the phenomenon of nonlinear oscillation.

A second-order autonomous system is represented by two scalar differential equa- tions

i . 1 = f 1 ( + 1 , z 2 ) (1 .28)

x2 = f 2 ( ~ 1 , ~ 2 ) (1 .29)

Let x ( t ) = ( z l ( t ) , z 2 ( t ) ) be the solution5 of (1.28)-(1.29) that starts at a certain initial state zo = ( x lo ,x zo ) ; that is, z ( 0 ) = z o . The locus in the 11-zz plane of the solution x ( t ) for all t > 0 is a curve that passes through the point xo . This curve is called a tmjectory or orbit of (1.28)-(1.29) from xo. The 2 1 - 2 2 plane is usually called the state plane or phase plane. The right-hand side of (1.28)-(1.29) expresses the tangent vector x ( t ) = ( i . ; ; l ( t ) , z z ( t ) ) to the curve. Using the vector notation

;= f ( z )

where f ( z ) is the vector ( f i ( z ) , f 2 ( z ) ) , we consider f ( z ) as a vector field on the state plane. This means that to each point z in the plane we assign a vector f ( x ) . For easy visualization, we represent f ( z ) as a vector based at x ; that is, we assign to z the directed line segment from z to z + f ( x ) . For example, if f ( x ) = ( 2 2 : , z 2 ) , then a t x = ( 1 , l ) we draw an arrow pointing from ( 1 , l ) to ( 1 , l ) + ( 2 , l ) = ( 3 , 2 ) ; see Figure 1.9. Repeating this at every point in the plane, we obtain the vector field diagram in Figure 1.10. In this figure, the length of the arrow at a given point z is proportional to J f ? ( z ) + f 2 ( z ) . Since the vector field at a point is tangent to the trajectory through that point, we can, in essence, construct the trajectory starting at a given point xo from the vector field diagram.

The family of all trajectories or solution curves is called the phase portrait of (1.28)-(1.29) . An (approximate) picture of the phase portrait can he constructed

51t is assumed that there is a unique solution.

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20 CHAPTER 1. INTRODUCTION

Figure 1.9: Vector field representation.

Figure 1.10: Vector field diagram.

by plotting trajectories from a large number of initial states spread all over the zl-zz plane. Since numerical subroutines for solving general nonlinear differential equations are widely available, we can easily construct the pbase portrait using computer simulation^.^ There are, however, several other methods for constructing the phase portrait. While we do not need to dwell on describing these methods, it might be useful to know one of them. Tbe method we chose to describe here is known as the isocline method. To understand the idea behind the method, note that the slope of a trajectory at any given point z, denoted by s(z), is given by

6Some hints for the construction of p h portraits using computer simulation arr given in Section 1.2.5.

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1.2. SECOND-ORDER SYSTEMS 21

Figure 1.11: Isocline with positive slope

Therefore, the equation s(x) = C

defines a curve in the XI-xz plane along which the trajectories of (1.28)-(1.29) have slope c. Thus, whenever a trajectory of (1.28)-(1.29) crosses the curve s(x) = c, the slope of the trajectory at the intersection point must be c. The procedure is to plot the curve s(x) = c in the XI-xz plane and along this curve draw short line segments having the slope c . These line segments are parallel and their directions are determined by the signs of f ~ ( x ) and fz(x) at x; see Figure 1.11. The curve s(x) = c is known as an isocline. The procedure is repeated for sufficiently many values of the constant c, until the plane is filled with isoclines. Then, starting from a given initial point xa, one can construct the trajectory from 2.0 by moving, in the direction of the short line segments, from one isocline to the next.

Example 1.1 Consider the pendulum equation without friction:

The slope function s(x) is given by

Hence, the isoclines are defined by

1 . xz = - - c sin XI

Figure 1.12 shows the isoclines for several values of c. One can easily sketch the trajectory starting at any point, as shown in the figure for the trajectory starting a t

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22 CHAPTER 1. INTRODUCTION

Figure 1.12: Graphical construction of the phase portrait of the pendulum equation (without friction) by the isocline method.

(rr/2,O). If the sketch is done carefully, one might even detect that the trajectory is a closed curve. Consider next the pendulum equation with friction

11 = 2 2

2 2 = - 0 . 5~2 -s in+,

This time the isoclines are defined by

1 x 2 = - - sin x1 0.5 + c

The isoclines shown in Figure 1.13 are identical to those of Figure 1.12, except for the slopes of the line segments. A sketch of the trajectory starting at ( ~ / 2 , 0 ) shows that the trajectory is a shrinking spiral that moves toward the origin. A

Note that since the time t is suppressed in a trajectory, i t is not possible to recover the solution (zl(t) , x2(t)) associated with a given trajectory. Hence, a tra- jectory gives only the qualatatrue but not quantrtatrue behavior of the associated

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1.2. SECOND-ORDER SYSTEMS 23

Figure 1.13: Graphical construction of the phase portrait of the pendulum equation (with friction) by the isocline method.

solution. For example, a closed trajectory shows that there is a periodic solution; that is, the system has a sustained oscillation, whereas a shrinking spiral shows a decaying oscillation. In the rest of this section, we will qualitatively analyze the behavior of second-order systems using their phase portraits.

1.2.1 Qualitative Behavior of Linear Systems

Consider the linear timeinvariant system

where A is a 2 x 2 real matrix. The solution of (1.30) for a given initial state zo is given by

z(t) = ~ e x ~ ( J , t ) ~ - ' z a

where J , is the real Jordan form of A and M is a real nonsingular matrix such that M-'AM = J,. Depending on the eigenvalues of A, the real Jordan form may take

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24 CHAPTER I . INTRODUCTION

one of the following three forms:

where k is either 0 or 1. The first form corresponds to the case when the eigenval- ues XI and A2 are real and distinct, the second form corresponds to the case when the eigenvalues are real and equal, and the third form corresponds to the case of complex eigenvalues A l , 2 = a + jp. In our analysis, we have to distinguish between these three cases. Moreover, in the case of real eigenvalues we have to isolate the case when at least one of the eigenvalues is zero. In that case, the origin is not an isolated equilibrium point and the qualitative behavior of the system is quite different from the other cases.

Case 1. Both eigenvalues are real: A1 # A2 # 0.

In this case, M = [ v l , v z ] where v l and v z are the real eigenvectors associated with A 1 and A z . The change of coordinates r = M-lz transforms the system into two decoupled first-order differential equations

whose solution, for a given initial state (210, zao), is given by

Eliminating t between the two equations, we obtain

where c = 2 2 0 / ( ~ 1 0 ) " ~ ~ ~ . The phase portrait of the system is given by the family of curves generated from (1.31) by allowing the constant c to take arbitrary values in R. The shape of the phase portrait depends on the signs of A1 and A2.

Consider first the case when both eigenvalues are negative. Without loss of generality, let A2 < A1 < 0. In this case, both exponential terms e A l * and $1'

tend to zero as t + m. Moreover, since A2 < A 1 < 0, the term e"' will tend to zero faster than the term e"'. Hence, we call A2 the fast eigenvalue and A1 the slow eigenvalue. For later reference, we call v2 the fast eigenvector and v l the slow eigenvector. The trajectory tends to the origin of the 21-12 plane along the curve (1.31), which now has a ratio & / A 1 that is greater than one. The slope of the curve is given by

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1.2. SECOND-ORDER SYSTEMS 25

Figure 1.14: Phase portrait of a stable node in modal coordinates

Figure 1.15: Phase h or traits for (a) a stable node; (b) an unstable node

Since [(X2/X1) - 11 is positive, the slope of the curve approaches zero as Jzl( -+ 0 and approaches m a s It11 i co. Therefore, as the trajectory approaches the origin, it becomes tangent to the zl-axis; as it approaches co, it becomes parallel to the 22-axis. These observations allow us to sketch the typical family of trajectories shown in Figure 1.14. When transformed hack into the x-coordinates, the family of trajectories will have the typical portrait shown in Figure 1.15(a). Note that in the X I - x a plane, the trajectories become tangent to the slow eigenvector vl as they approach the origin and parallel to the fast eigenvector vz far from the origin. In this case, the equilibrium point x = 0 is called a stable node.

When XI and X z are positive, the phase portrait will retain the character of Fig- ure 1.15(a) hut with the trajectory directions reversed, since the exponential terms eA" and eAat grow exponentially as t increases. Figure 1.15(b) shows the phase portrait for the case X z > XI > 0. The equilibrium point I = 0 is referred to in this

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26 CHAPTER 1. INTRODUCTION

Figure 1.16: Phase portrait of a saddle point (a) in modal coordinates; (b) in original coordinates.

case as an unstable node.

Suppose now that the eigenvalues have opposite signs. In particular, let A* < 0 < XI. In this case, eA1' -r w while eA2' + 0 as t -+ w. Hence, we call A z the stable eigenvalue and A1 the unstable eigenvalne. Correspondingly, uz and ul are called the stable and unstable eigenvectors, respectively. The trajectory equation (1.31) will have a negative exponent (Az/Al). Thus, the family of trajectories in the zl-rz plane will take the typical form shown in Figure 1.16(a). Trajectories have hyperbolic shapes. They become tangent to the 21-axis a s lzl( i m and tangent to the 22-axis as lrll --t 0. The only exception to these hyperbolic shapes are the four trajectories along the axes. The two trajectories along the 22-axis are called the sta- ble trajectories since they approach the origin as t -r w, while the two trajectories along the 21-axis are called the unstable trajectories since they approach infinity as t + m. The phase portrait in the XI-xz plane is shown in Figure 1.16(h). Here the stable trajectories are along the stable eigenvector v2 and t,he unstable trajectories are along the unstable eigenvector 01. In this case, the equilibrium point is called a saddle.

Case 2. Complex eigenvalues: Al ,z = a f jp.

The change of coordinates z = M-lx transforms the system (1.30) into the form

The solution of this equation is oscillatory and can be expressed more conveniently

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1.2. SECOND-ORDER SYSTEMS 27

Figure 1.17: Typical trajectories in the case of complex eigenvalues (a) a < 0; (b) a > 0; (c) a = 0.

Figure 1.18: Phase portraits for (a) a stable focus; (b) an unstable focus; (c) a center.

in the polar coordinates

where we have two uncoupled first-order differential equations:

The solution for a given initial state ( ro , 90) is given by

~ ( t ) = roe"', B(t) = 00 + pt

which defines a logarithmic spiral in the 21-22 plane. Depending on the value of a, the trajectory will take one of the three forms shown in Figure 1.17. When a < 0, the spiral converges to the origin; when a > 0, it diverges away from the origin. When a = 0, the trajectory is a circle of radius TO. Figure 1.18 shows the trajecto- ries in the z,-zz plane. The equilibrium point z = 0 is referred to as a stable focus if a < 0 , unstable focus if a > 0, and cenier if a = 0.

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28 CHAPTER 1. INTRODUCTION

Figure 1.19: Phase portraits for the case of nonzero multiple eigenvalues when k = 0: (a) A < 0; (b) A > 0.

Case 3. Nonzero mul t ip le eigenvalues: XI = A2 = X # 0.

The change of coordinates z = M - ' z transforms the system (1.30) into the form

f l = Azl + kz2

t 2 = Xz2

whose solution, for a given initial state (zla, zzo), is given by

z l ( t ) = e"(z10 + kzzot), zz(t) = eAtzzo

Eliminating t , we obtain the trajectory equation

Figure 1.19 shows the form of the trajectories when k = 0, while Figure 1.20 shows their form when k = 1. The phase portrait has some similarity with the portrait of a node. Therefore, the equilibrium point x = 0 is usually referred t o as a stable node if A < 0 and unstable node ifA > 0. Note, however, that the phase portraits of Figures 1.19 and 1.20 do not have the asymptotic slow-fast behavior that we saw in Figures 1.14 and 1.15.

Before we discuss the degenerate case when one or both of the eigenvalues are zero, let us summarize our findings about the qualitative behavior of the system when the equilibrium point x = 0 is isolated. We have seen that the system can dis- , . play six qualitatively different phase portraits, which are associated with different types of equilibria: stable node, unstable node, saddle point, stable focus, unstable focus, and center. The type of equilibrium point is completely specified by the lo- cation of the eigenvalues of A. Note that the global (throughout the phase plane)

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1.2. SECOND-ORDER SYSTEMS 29

Figure 1.20: Phase or traits for the case o f nonzero multiple eigenvalues when k = 1: (a) A < 0; (b) X > 0.

qualitative behavior of the system is determined by the type of equilibrium point. This is a characteristic of linear systems. Wheu we study the qualitative behavior of nonlinear systems in the next section, we shall see that the type of equilibrium point can only determine the qualitative behavior of the trajectories in the vicinity of that point.

Case 4. One or both eigenvalues are zero.

Wheu one or both eigenvalues of A are zero, the phase portrait is in some sense degenerate. In this case, the matrix A has a nontrivial null space. Any vector in the null space of A is an equilibrium point for the system; that is, the system has an equilibrium subspace rather than an equilibrium point. The dimension of the null space could be one or two; if it is two, the matrix A will be the zero matrix. This is a trivial case where every point in the plane is an equilibrium point. When the dimension of the null space is one, the shape of the Jordan form of A will depend on the multiplicity of the zero eigenvalue. When XI = 0 and X z # 0,the matrix M is given by M = [ul, u2] where u l and uz are the associated eigenvectors. Note that vl spans the null space of A. The change of variables 2 = M- ' z results in

whose solution is q ( t ) = +lo , 12(t) = t2oeAa'

The exponential term will grow or decay, depending on the sign of X2. Figure 1.21 shows the phase portrait in the XI-22 plane. All trajectories converge to the equi- librium subspace when A2 < 0, and diverge away from it when X2 > 0.

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30 CHAPTER 1 . INTRODUCTION

(a) (b)

Figure 1.21: Phase portraits for (a) X~ = 0, ,I? < 0; (b) X~ = 0, X~ > 0

Figure 1.22: Phase portrait when XI = X 2 = 0.

When both eigenvalues are a t the origin, the change of variables z = M-'c results in

whose solution is

z1(t) = 210 + zzot. zz(t) = z20

The term zzot will increase or decrease, depending on the sign of rzo. The 21-axis is the equilibrium subspace. Figure 1.22 shows the phase portrait in the XI-cz plane; the dashed line is the equilibrium subspace. The phase portrait in Figure 1.22 is quite different from that in Flgure 1.21. Trajectories starting off the equilibrium subspace move parallel to it.

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1.2. SECOND-ORDER SYSTEMS 31

The study of the behavior of linear systems about the equilibrium point x = 0 is important because, in many cases, the local behavior of a nonlinear system near an equilibrium point can be deduced by linearizing the system about that point and studying the behavior of the resultant linear system. How conclusive this approach is depends to a great extent on how the various qualitative phase portraits of a linear system persist under perturbations. We can gain insight into the behavior of a linear system under perturbations by examining the special case of linear per- turbations. Suppose A has distinct eigenvalues and consider A + AA, where A A is a 2 x 2 real matrix whose elements have arbitrarily small magnitudes. From the perturbation theory of matrices,' we know that the eigenvalues of a matrix depend continuously on its parameters. This means that, given any positive number r , there is a corresponding positive number 6 such that if the magnitude of the perturbation in each element of A is less than 6, the eigenvalues of the perturbed matrix A + A A will lie in open balls of radius r centered at the eigenvalues of A. Consequently, any eigenvalue of A which lies in the open right-half plane (positive real part) or in the open left-half plane (negative real part) will remain in its respective half of the plane after arbitrarily small perturbations. On the other hand, eigenvalues on the imaginary axis, when perturbed, might go into either the right-half or the left-half of the plane since a ball centered on the imaginary axis will extend in both halves no matter how small E is. Consequently, we can conclude that if the equilibrium point x = 0 of x = Ax is a node, focus, or saddle point, then the equilibrium point x = 0 of = (A+AA)x will be of the same type for sufficiently small perturbations. The situation is quite different if the equilibrium point is a center. Consider the following perturbation of the real Jordan form in the case of a center

where p is a perturbation parameter. When p is positive, the equilibrium point of the perturbed system is an unstable focus; when p is negative it is a stable focus. This is true no matter how small p is, as long as it is different from zero. Because the phase portraits of a stable focus and unstable focus are qualitatively different from the phase portrait of a center, we see that a center equilibrium point will not persist under perturbations. The node, focus, and saddle equilibrium points are said to be structurally stable because they maintain their qualitative behavior under infinitesimally small perturbation^,^ while the center equilibrium point is not structurally stable. The distinction between the two cases is due to the location of the eigenvalues of A, with the eigenvalues on the imaginary axis being vulnerable to perturbations. This brings in the definition of a hyperbolic equilibrium point. The origin x = 0 is said to be a hyperbolic equilibrium point of x = Ax if A has no

'See 157, Chapter 71. 'See [70, Chapter 161 for a rigorous and more general definition of structural stability

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32 CHAPTER 1. INTRODUCTION

Figure 1.23: Phase portraits of a perturbed system when XI = 0 and Xz < 0: (a) p < 0; (b) p > 0.

eigenvalues with zero real part.' When A has multiple nonzero real eigenvalues, infinitesimally small per turbs

tions could result in a pair of complex eigenvalues. Hence, a stable (respectively, unstable) node would either remain a stable (respectively, unstable) node or become a stable (respectively, unstable) focus.

When A has eigenvalues at zero, one would expect perturbations to move these eigenvalues away from zero, resulting in a major change in the phase portrait. It turns out, however, that there is an important difference between the case when there is only one eigenvalue a t zero and the case when both eigenvalues are at zero ( A f 0). In the first case, perturbation of the zero eigenvalue results in a reid eigenvalue XI = p where p could be positive or negative. Since the other eigenvalue Xz is different from zero, its perturbation will keep it away from zero. Moreover, since we are talking about arbitrarily small perturbations, /XI) = (p1 will be much smaller than IXzl. Thus, we end up with two real distinct eigenvalues, which means that the equilibrium point of the perturbed system will be a node or a saddle point, depending on the signs of and p. This is already an important change in the phase portrait. However, a careful examination of the phase portrait gives more insight into the qualitative behavior of the system. Since (XI( << (Xz(, the exponential term eA2' will change with t much faster than the exponential term e h t . This results in the typical phase portraits of a node and a saddle shown in Figure 1.23, for the case Xz < 0. Comparison of these phase portraits with Figure 1.21(a) shows some similarity. In particular, similar to Figure 1.21, trajectories starting off the eigenvector v l converge to that vector along lines (almost) parallel to the eigenvector vz. As they approach the vector v l , they become tangent to it and move along it.

sThis definition of a hyperbolic equilibrium point extends to higher-dimensional systems. It also carries over to equilibriaof nonlinear systems by applying it to the eigenvaluesof the linearized system.

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1.2. SECOND-ORDER SYSTEMS 33

When p < 0, the motion along vl converges to the origin (stable node) while when p > 0 the motion along vl tends to infinity (saddle point). This qualitative behavior is characteristic of singularly perturbed systems, which will be studied in Chapter 9.

When both eigenvalues of A are zeros, the effect of perturbations is more dra- matic. Consider the following four possible perturbations of the Jordan form:

where p is a perturbation parameter which could he positive or negative. It can be easily seen that the equilibrium points in these four cases are a center, a focus, a node, and a saddle point, respectively. In other words, all the possible phase portraits of an isolated equilibrium could result from perturbations.

1.2.2 Multiple Equilibria

The linear system (1.30) has an isolated equilibrium point a t x = 0 if A has no zero eigenvalues, that is, if det A # 0. When det A = 0, the system has a continuum of equilibrium points. These are the only possible equilibria patterns that a linear system may have. A nonlinear system can have multiple isolated equilibrium points. In the following two examples, we explore the qualitative behavior of the tunnel diode circuit of Section 1.1.2 and the pendulum equation of Section 1.1.1. Both systems exhibit multiple isolated equilibria.

Example 1.2 The state-space model of a tunnel diode circuit is given by

Assume the circuit parameters are1' u = 1.2 V , R = 1.5 kR = 1.5 x lo3 a, C = 2 pF = 2 x 10-l2 F, and L = 5 pH = 5 x N. Measuring time in nanoseconds and the currents x2 and h(x1) in mA, the state-space model is given by

Suppose h(.) is given by

h(xl) = 1 7 . 7 6 ~ ~ - 103.791: + 229.621; - 226.31xt+ 83.722:

'"The numerical data are taken from 133).

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34 CHAPTER 1. INTRODUCTION

Figure 1.24: Phase portrait of the tunnel diode circuit o f Example 1.2.

Setting 21 = i.2 = 0 and solving for the equilibrium points, i t can be verified that there are three equilibrium points a t (0.063,0.758), (0.285,0.61), and (0.884,0.21). The phase portrait of the system, generated by a computer program, is shown in Figure 1.24. The three equilibrium points are denoted in the portrait by Q1, Q2, and Q3, respectively. Examination of the phase portrait shows that, except for two special trajectories which tend t o the point Qz, all trajectories eventually tend to either the point Q1 or the point Q 3 . The two special trajectories converging to Qz form a curve that divides the plane into two halves. All trajectories originating from the left side of the curve will tend to the point Q1, while all trajectories originating from the right side will tend to point Q3. This special curve is called a separatrix because it partitions the plane into two regions of different qualitative behavior." In an experimental setup, we shall observe one of the two steady-state operating points Q1 or Q3, depending on the initial capacitor voltage and inductor current. The equilibrium point a t Qz is never observed in practice because the ever-present physical noise would cause the trajectory to diverge from Q2 even if i t were possible to set up the exact initial conditions corresponding to Qz. This tunnel

"In general, the state plane decomposes into a number of regions, within each of which the trajectories may show a different type of behavior. The curves separating these regions are called separatrices.

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1.2. SECOND-ORDER SYSTEMS

Figure 1.25: Adjustment of the load line of the tunnel diode circuit during triggering.

diode circuit with multiple equilibria is referred to as a baslable circuit, because it has two steady-state operating points. I t has been used as a computer memory, where the equilibrium point Ql is associated with the binary state "0" and the equilibrium point Q3 is associated with the binary state "1." Triggering from Q1 to Q3 or vice versa is achieved by a triggering signal of sufficient amplitude and duration which allows the trajectory to move to the other side of the separatrix. For example, if the circuit is initially a t Q , , then a positive pulse added to the supply voltage u will carry the trajectory to the right side of the separatrix. The pulse must be adequate in amplitude to raise the load line beyond the dashed line in Figure 1.25 and long enough to allow the trajectory to reach the right side of the separatrix.

The phase portrait in Figure 1.24 tells us the global qualitative behavior of the tunnel diode circuit. The range of x 1 and x2 was chosen so that all essential qualitative features are displayed. The portrait outside this range does not contain any new qualitative features. A

Example 1.3 Consider the pendulum equation with friction:

A computer-generated phase portrait for g / l = 1 and k / m = 0.5 is shown in Fig- ure 1.26. The phase portrait is periodic with a period equal to 2 ~ . Consequently, all distinct features of the system's qualitative behavior can be captured by drawing the portrait in the vertical strip -rr < xl 5 rr, as shown in Figure 1.27. To follow a trajectory starting from an arbitrary initial state, we may have to switch back

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36 CHAPTER 1 . INTRODUCTION

' O r -

Figure 1.26: Phase portrait of the pendulum equation of Example 1.3

and forth between the vertical boundaries of this strip. For example, consider the trajectory starting from point a in Figure 1.27. Follow this trajectory until i t hits the right boundary a t point b; then identify point c on the left boundary, which has the same value of the 2 2 coordinate as point b . We then continue following the trajectory from c. This process is equivalent to following the trajectory on a cylinder formed by cutting out the phase portrait in Figure 1.27 along the vertical lines zl = f a and pasting them together. When represented in this manner, the pendulum equation is said to be represented in a cylindrical phase space rather than a phase plane. From the phase portrait we see that, except for special trajectories which terminate a t the "unstable" equilibrium position (a, 0), all other trajectories tend to the "stable" equilibrium position (0,O). Once again, the "unstable" equi- librium position (a, 0) cannot be maintained in practice, because noise would cause the trajectory to diverge away from that position. A

1.2.3 Qualitative Behavior Near Equilibrium Points

Examination of the phase portraits in Examples 1.2 and 1.3 shows that the qualita- tive behavior in the vicinity of each equilibrium point looks just like those we saw in Section 1.2.1 for linear systems. In particular, in Figure 1.24 the trajectories near

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1.2. SECOND-ORDER SYSTEMS 37

Figure 1.27: Phase portrait of the pendulum equation over the region-?r 5 z1 5 r.

Q l , Q2, and Q3 are similar to those associated with a stable node, saddle point, and stable node, respectively. Similarly, in Figure 1.26 the trajectories near (0,O) and (r,O) are similar to those associated with a stable focus and a saddle point, respectively. These observations are actually quite general. Except for some special cases, the qualitative behavior of a nonlinear system near an equilibrium point can be determined via linearization with respect to that point.

Let p = (pl,p2) be an equilibrium point of the nonlinear system (1.28)-(1.29), and suppose that the functions fl and f2 are continuously differentiable. Expanding the right-hand side of (1.28)-(1.29) into its Taylor series about the point (pl,pz), we obtain

where

and H.O.T. denotes higher-order terms of the expansion, that is, terms of the form (21 -PI)= , ( ~ 2 - p ~ ) ~ , (XI-pl ) x (x2 -m) , and so on. Since (pl,p2) is an equilibrium point, we have

f l ( ~ l , ~ 2 ) = f 2 ( ~ 1 > ~ 2 ) = 0 Moreover, since we are interested in the trajectories near (pl,pz), we define

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38 CHAPTER 1. INTRODUCTION

and rewrite the state equation as

= X I = a l l y , + alzyz + H.O.T.

~2 = ~2 = a 2 1 y 1 + azzy2 + H.O.T.

If we restrict attention to a sufficiently small neighborhood of the equilibrium point such that the higher-order terms are negligible, then we may drop these terms and approximate the nonlinear state equation by the linear state equation

Rewriting this equation in a vector form, we obtain

where

The matrix [ 8 f / a x ] is called the Jacobian matrix of f(x) and A is the Jacobian matrix evaluated at the equilibrium point p.

It is reasonable to expect that the trajectories of the nonlinear system in a small neighborhood of an equilibrium point are "close" to the trajectories of its lineariza- tion about that point. Indeed it is true thatr2 if the origin of the linearized state equation is a stable (respectiuely, unstable) node with distinct eigenualues, a stable (respectively, unstable) focus, or a saddle point, then, in a small neighborhood of the equilibrium point, the trajectories of the nonlinear state equation will behave like a stable (respectiuely, unstable) node, a stable (respectiuely, unstable) focus, o r a saddle point. Consequently, we call an equilibrium point of the nonlinear state equation (1.28)-(1.29) a stable (respectively, unstable) node, a stable (respectively, unstable) focus, or a saddle point if its linearized state equation about the equilih- rium point has the same behavior. The type of equilibrium points in Examples 1.2 and 1.3 could have been determined by linearization without the need to construct the global phase portrait of the system.

''The proof of this linearization property can be found in [66]. It is "did under the assumption that .fl(zl ,a) and fi(zl.zz) have continuous first partial derivatives in a neighborhood of the equilibrium point ( P I . PZ). A related, but different, linearization result will be proved in Chapter 3 for higher-dimensional systems; see Theorem 3.7.

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1.2. SECOND-ORDER SYSTEMS 39

Example 1.4 The Jacobian matrix of the function f (z) of the tunnel diode circuit in Example 1.2 is given by

where

Evaluating the Jacobian matrix at the equilibrium points QI = (0.063,0.758), Qz = (0.285,0.61), and Q3 = (0.884,0.21), respectively, yields the three matrices

Eigenvalues : - 3.57, -0.33

Eigenvalues : 1.77, -0.25

A3 = [ -1.427 0.5 Eigenvalues: - 1.33, -0.4

Thus, Q1 is a stable node, Q2 is a saddle point, and Q3 is a stable node. A

Example 1.5 The Jacobian matrix of the function f(z) of the pendulum equation in Example 1.3 is given by

Evaluating the Jacobian matrix at the equilibrium points (0,O) and (r,0) yields, respectively, the two matrices

1 '1 = [ !l 0 . 5 1 , Eigenvalues : - 0.25 i j0.97

Eigenvalues : - 1.28, 0.78

Thus, the equilibrium point (0,O) is a stable focus and the equilibrium point (?r, 0) is a saddle point. A

Note that the foregoing linearization property dealt only with cases when the linearized state equation has no eigenvalues on the imaginary axis, that is, when the origin is a hyperbolic equilibrium point of the linear system. We extend this

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40 CHAPTER 1. INTRODUCTION

definition to nonlinear systems and say that an equilibrium point is hyperbolic if the Jacobian matrix, evaluated at that point, has no eigenvalues on the imaginary axis. If the Jacobian matrix has eigenvalues on the imaginary axis, then the qual- itative behavior of the nonlinear state equation near the equilibrium point could be quite distinct from that of the linearized state equation. This should come as no surprise in view of our earlier discussion on the effect of linear perturbations on the qualitative behavior of a linear system when the origin is not a hyperbolic equilibrium point. The following example considers a case when the origin of the linearized state equation is a center.

Example 1.6 The system

has an equilibrium point at the origin. The linearized state equation at the origin has eigenvalues * j . Thus, the origin is a center equilibrium point for the linearized system. In this particular example, we can determine the qualitative behavior of the nonlinear system by representing the system in polar coordinates:

z1 = r cos 8 , 2 2 = r sin 8

which yields i = -11r3, 8 = 1

From these equations, it can be easily seen that the trajectories of the nonlinear system will resemble a stable focus when p > 0 and an unstable focus when 11 < 0.

A ,

This example shows that the qualitative behavior describing a center in the linearized state equation is not preserved in the nonlinear state equation.

The foregoing discussion excludes the case when the linearized state equation has a node with multiple eigenvalues. Exercise 1.15 shows a case where the linearization has a stable node, while the trajectories of the nonlinear state equation behave like a stable focus. It should be mentioned, however, that a smoother function f ( z ) will not allow this to happen. In particular, if f l ( z l , z z ) and f 2 ( z l , z 2 ) are analytic functionsi3 in a neighborhood of the equilibrium point, then it is true thati4 if the origin of the linearized state equation i s a stable (respectively, unstable) node, then, i n a small neighborhood of the equilibrium point, the trajectories of the nonlinear state equation will behave like a stable (respectively, unstable) node whether or not the eigenvalues of the linearization are distinct.

I3That is, fi and fi have convergent Taylor series representations. "See 1102, Theorem 3.4, page 1881.

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1.2. SECOND-ORDER SYSTEMS 41

Determining the type of equilibrium points via linearization provides useful in- formation that should he used when we construct a global phase portrait of a second-order system, whether we do that graphically or numerically. In fact, the first step in constructing a phase portrait should he the calculation of all equilibrium points and determining the type of isolated ones via linearization. This will give us a clear idea about the expected portrait in the neighborhood of the equilihrium points.

1.2.4 Limit Cycles

Oscillation is one of the most important phenomena that occur in dynamical sys- tems. A system oscillates when it has a nontrivial periodic solution

for some T > 0. The word "nontrivial" is used to exclude constant solutions cor- responding to equilihrium points. A constant solution satisfies the above equation, hut it is not what we have in mind when we talk of oscillation or periodic solutions. Unless otherwise specified, from this point on whenever we refer to a periodic solu- tion we shall mean a nontrivial one. The image of a periodic solution in the phase portrait is a closed trajectory, that is usually called a periodic orbit or a closed orbit.

We have already seen an example of oscillation in Section 1.2.1: the second-order linear system with eigenvalues ijp. The origin of that system is a center, and the trajectories are closed orbits. When the system is transformed into its real Jordan form, the solution is given by

where

To = d m , 00 = tan- I [-] Therefore, the system has a sustained oscillation of amplitude TO. It is usually re- ferred to as the harmonic oscillator. If we think of the harmonic oscillator as a model for the linear LC circuit of Figure 1.28, then we can see that the physical mechanism leading to these oscillations is a periodic exchange (without dissipation) of the energy stored in the capacitor electric field with the energy stored in the inductor magnetic field. There are, however, two fundamental problems with this linear oscillator. The first problem is one of robustness. We have seen that in- finitesimally small right-hand side (linear or nonlinear) perturbations will destroy the oscillation. That is, the linear oscillator is not structurally stable. In fact, it is impossible to build an LC circuit that realizes the harmonic oscillator, for the resistance in the electric wires alone will eventually consume whatever energy was

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Figure 1.28: A linear LC circuit for the harmonic oscillator.

initially stored in the capacitor and inductor. Even if we succeeded in building this linear oscillator, we would face the second problem: the amplitude of oscillation is dependent on the initial conditions.

The two fundamental problems of the linear oscillator can be eliminated in nonlinear oscillators. It is possible to build physical nonlinear oscillators such that

The nonlinear oscillator is structurally stable

The amplitude of oscillation (at steady state) is independent of initial condi- tions.

The negative-resistance oscillator of Section 1.1.4 is an example of such nonlinear oscillators. The state equation of the system is given by

where the function h satisfies certain properties, stated in Section 1.1.4. The system has only one equilibrium point a t XI = zz = 0. The Jacohian matrix a t this point is given by

0

-1 -chl(0) ' I Since hi(0) < 0, the origin is either an unstable node or unstable focus depending on the value of ch1(O). In either case, all trajectories starting near the origin would diverge away from it and head toward infinity. This repelling feature of the origin is due t o the negative resistance of the resistive element near the origin, which means that the resistive element is "active" and supplies energy. This point can be seen analytically by writing an expression for the rate of change of energy. The total energy stored in the capacitor and inductor a t any time t is given by

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1.2. SECOND-ORDER SYSTEMS 43

Figure 1.29: A sketch of h(xl) (solid) and -xlh(xl) (dashed) which shows that E is positive for -a 5 XI 5 b.

We have seen in Section 1.1.4 that

Thus, recalling that r = m, we can rewrite the energy expression as

E = ${xf + [eh(xl) + x-L]'}

The rate of change of energy is given by

This expression confirms that, near the origin, the trajectory gains energy since for small (x l ( the term xlh(xl) is negative. It also shows that there is a strip -a 5 X I < b such that the trajectory gains energy within the strip and loses energy outside the strip. The strip boundaries -a and 6 are roots of h(xl) = 0, as shown in Figure 1.29. As a trajectory moves in and out of the strip, there is an exchange of energy with the trajectory gaining energy inside the strip and losing it outside. A stationary oscillation will occur if, along a trajectory, the net exchange of energy over one cycle is zero. Such a trajectory will be a closed orbit. It turns out that the negative-resistance oscillator has an isolated closed orbit, which is illustrated in the next example for the Van der Pol oscillator.

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44 CHAPTER 1. INTRODUCTION

Figure 1.30: Phase portraits of the Van der Pol oscillator: (a) r = 0.2; (b) r = 1.0.

Figure 1.31: Phase portrait of the Van der Pol oscillator with r = 5.0: (a) in 2,-z2 plane; (b) in 21-22 plane.

Example 1.7 Figures 1.30(a), 1.30(b), and 1.31(a) show the phase portraits of the Van der Pol equation

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1.2. SECOND-ORDER SYSTEMS 45

Figure 1.32: (a) A stable limit cycle; (b) an unstable limit cycle.

revealing phase portrait in this case can be obtained when the state variables are chosen as z1 = i~ and z2 = vc, resulting in the state equation

The phase portrait in the zt-zz plane for e = 5.0 is shown in Figure 1.31(b). The closed orbit is very close t o the curve zl = z2 - gz; except a t the corners, where it becomes nearly vertical. This vertical portion of the closed orbit can he viewed as if the closed orbit jumps from one branch of the curve to the other as i t reaches the corner. Oscillations where this jump phenomenon takes place are usually referred to as relaxation oscillations. This phase portrait is typical for large values of E (say, E > 3.0). a

The closed orbit we have seen in Example 1.7 is different from what we have seen in the harmonic oscillator. In the case of the harmonic oscillator, there is a continuum of closed orbits, while in the Van der Pol example there is only one isolated periodic orbit. An isolated periodic orbit is called a limit cycle.15 The limit cycle of the Van der Pol oscillator has the property that all trajectories in the vicinity of the limit cycle ultimately tend toward the limit cycle as t -+ co. A limit cycle with this property is classically known as a stable limit cycle. We shall also encounter unstable limit cycles, which have the property that all trajectories starting from points arbitrarily close to the limit cycle will tend away from it as t - w; see Figure 1.32. To see an example of an unstable limit cycle, consider the Van der Pol equation in reverse time; that is,

I 5 A formal definition of limit cycles will be given in Chapter 6.

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46 CHAPTER 1. INTRODUCTION

The phase portrait of this system is identical to that of the Van der Pol oscillator, except that the arrowheads are reversed. Consequently, the limit cycle is unstable.

The limit cycle of the Van der Pol oscillator of Example 1.7 takes special forms in the limiting cases when c is very small and very large. These special forms can be predicted analytically using asymptotic methods. In Chapter 8, we shall use the averaging method to derive the special form of the limit cycle as r --t 0, while in Chapter 9 we shall use the singular perturbation method to derive the special form of the limit cycle as r --t co.

1.2.5 Numerical Construction of Phase Portraits

Computer programs for numerical solution of ordinary differential equations are widely available. They can be effectively used to construct phase portraits for second-order systems. In this section, we give some hintsI6 that might be useful for beginners.

The first step in constructing the phase portrait is to find all equilibrium points and determine the type of isolated ones via linearization.

Drawing trajectories involves three tasks:"

Selection of a bounding box in the state plane where trajectories are to be drawn. The box takes the form

Selection of initial points (conditions) inside the bounding box.

Calculation of trajectories.

Let us talk first about calculating trajectories. To find the trajectory passing through a point xo, solve the equation

in forward time (with positive t) and in reverse time (with negative t ) . Solution in reverse time is equivalent to solution in forward time of the equation

x = -f(x), x(0) = x,

16These hints are taken from [132, Chapter 101, which contains more instructions on how to generate informative phase portraits.

' 7 A fourth task that we left out is placing arrowheads on the trajectory. For the purpose of this textbook, this can be conveniently done manually.

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1.3. EXERCISES 47

since the change of time variable T = -t reverses the sign of the right-hand side. The arrowhead on the forward trajectory is placed heading away from zo, while the one on the reverse trajectory is placed heading into zo. Note that solution in reverse time is the only way we can get a good portrait in the neighborhood of unstable focus, unstable node, or unstable limit cycle. Trajectories are continued until they get out of the bounding box. If processing time is a concern, you may want to add a stopping criterion when trajectories converge to an equilibrium point.

The bounding box should be selected so that all essential qualitative features are displayed. Since some of these features will not be known a priorz, we may have to adjust the bounding box interactively. However, our initial choice should make use of all prior information. For example, the box should include all equilibrium points. Care should he exercised when a trajectory travels out of bounds, for such a trajectory is either unbounded or is attracted to a stable limit cycle.

The simplest approach to select initial points is to place them uniformly on a grid throughout the bounding box. However, an evenly spaced set of initial conditions rarely yields an evenly spaced set of trajectories. A better approach is t o select the initial points interactively after plotting the already calculated trajectories. Since most computer programs have sophisticated plotting tools, this approach should he quite feasible.

For a saddle point, we can use linearization to generate the stable and unstable trajectories. This is useful because, as we saw in Examples 1.2 and 1.3, the stable trajectories of a saddle define a separatrix. Let the eigcnvalucs of the linearization be XI > 0 > Xz, and the corresponding eigenvectors be vl and vz. The stable and unstahle trajectories of the nonlinear saddle will be tangent to the stable eigenvector vz and the unstable eigenvector v l , respectively, as they approach the equilibrium point p. Therefore, the two unstahle trajectories can be generated from the initial points zo = p f av l , where a is a small positive number. Similarly, the two stable trajectories can be generated from the initial points zo = pf a v z . The major patts of the unstable trajectories will be generated by solution in forward time, while the major parts of the stable ones will be generated by solution in reverse time.

1.3 Exercises

Exercise 1.1 A mathematicalmodel that describes a wide variety of physical non- linear systems is the nth-order differential equation

where u and y are scalar variables. With u as input and y as output, find a state- space model.

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48 CHAPTER 1. INTRODUCTION

Exercise 1.2 Consider a singlf-input-single-output system described by the nth- order differential equation

where g2(,) is a differentiable function of its arguments. With u as input and y as output, find a state-space model.

Hint: Take z, = - g2

Exercise 1.3 The nonlinear dynamic equations for an m-link rohot [I661 take the form

M(q)i ; + c(n, d 4 + s ( q ) = u

where q is an m-dimensional vector of generalized coordinates representing joint positions, u is an m-dimensional control (torque) input, and M ( q ) is a symmetric inertia matrix which is positive definite V q E Rm. The term C ( q , q)q aFcounts for centrifugal and Coriolis forces. The matrix C has the property that M - 2C is a skew-symmetric matrix V q, q E Rm, where M is the total derivative of M ( q ) with respect to t . The term g(q) , which accounts for gravity forces, is given by g(q) = [aP(q ) /aqIT , where P ( q ) is the total potential energy of the links due to gravity. We assume that P ( q ) is a positive definite function of q , and g(q) = 0 has an isolated root at q = 0." Choose state variables for this system and write down the state equation.

Exercise 1.4 The nonlinear dynamic equations for a single-link manipulator with flexible joints [166], damping ignored, is given by

where q1 and 92 are angular positions, I and J are moments of inertia, P is a spring constant, M is the total mass, L is a distance, and u is a torque input. Choose state variables for this system and write down the state equation.

Exercise 1.5 The nonlinear dynamic equations for an m-link rohot with flexible joints 11661 take the form

''The properties of C. M, and P are not needed in this exercise. They will be used in later exercises.

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1.3. EXERCISES 49

Nonlmear Y Element

Figure 1.33: Exercise 1.6

where ql and qz are m-dimensional vectors of generalized coordinates, M(q1) and J are symmetric nonsingular inertia matrices, and u is an m-dimensional control input. The term h(q, q) accounts for centrifugal, Coriolis, and gravity forces, and K is a diagonal matrix of joint spring constants. Choose state variables for this system and write down the state equation.

Exercise 1.6 Figure 1.33 shows a feedback connection of a linear time- invariant system and a nonlinear time-varying element. The variables r, u, and y are vectors of the same dimension, and ~ ( t , y) is a vector-valued function. With T as input and y as output, find a state-space model.

Exercise 1.7 A synchronous generator connected to an infinite bus can be repre- sented [I311 by

where 6 is an angle in radians, Eq is voltage, P is mechanical input power, EFD is field voltage (input), D is damping coefficient, M is inertial coefficient, r is a time constant, and 71, qz, and q3 are constant parameters.

(a) Using 6, 6, and E, as state variables, find the state equation.

(b) Let P = 0.815, EFD = 1.22, 71 = 2.0, qz = 2.7, q3 = 1.7, r = 6.6, M = 0.0147, and D I M = 4. Find all equilibrium points.

(c) Suppose that r is relatively large so that Eq GS 0. Show that assuming Eq to be constant reduces the model to a pendulum equation.

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50 CHAPTER 1. INTRODUCTION

Figure 1.34: Exercises 1.8 and 1.9.

Exercise 1.8 The circuit shown in Figure 1.34 contains a nonlinear inductor and is driven by a timedependent current source. Suppose that the nonlinear inductor is a Josephson junction [33], described by i ~ = l o sin t 4 ~ where 4~ is the magnetic flux of the inductor and 10 and ic are constants.

(a ) Using 4~ and vc as state variables, find the state equation

(b ) Is i t easier t o choose i ~ and vc as state variables?

Exercise 1.9 The circuit shown in Figure 1.34 contains a nonlinear inductor and is driven by a timedependent current source. Suppose that the nonlinear inductor is described by i ~ = L ~ L + p 4 ; , where 4~ is the magnetic flux of the inductor and L and p are positive constants.

(a ) Using 4~ and vc as state variables, find the state equation.

( b ) Let i , = 0. Find all equilibrium points and determine the type of each point

Exercise 1.10 A phase-locked loop [54] can be represented by the block diagram of Figure 1.35. Let {A, B, C ) be a minimal realization of the scalar, strictly proper, mth-order transfer function G(s). Assume that all eigenvalues of A have negative real parts, G(0) # 0, and 0, = constant. Let z be the state of the realization { A , B, C) .

(a) Show that the closed-loop system can be represented by the state equation

( b ) Find all equilibrium points of the system

(c) Show that when G(s) = l/(rs + l), the closed-loop model coincides with the model of a pendulum equation.

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1.3. EXERCISES 51

Figure 1.35: Exercise 1.10.

"'7

Figure 1.36: Exercise 1.11

Exercise 1.11 Consider the mass-spring system shown in Figure 1.36. Assuming a linear spring and nonlinear viscous damping described by clG+czylyl, find a state equation that describes the motion of the system.

Exercise 1.12 A field-controlled DC motor 11591 can be described by

di. u. = c l i p + Lo- dt + R.i,

The first equation is for the field circuit with u l , i t , R I , and Lf being its voltage, current, resistance, and inductance. The variables u,, i,, R., and L, are the corre- sponding variables for the armature circuit described by the second equation. The

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52 CHAPTER I. INTRODUCTION

third equation is a torque equation for the shaft, with J as the rotor inertia and cs as damping coefficient. The term clifw is the back e.m.f. induced in the armature circuit, and c2if i, is the torque produced by the interaction of the armature cur- rent with the field circuit flux. The voltage v. is held constant, and the voltage vf is the control input. Choose appropriate state variables and write down the state equation.

Exercise 1.13 For each of the following systems, find all equilibrium points and determine the type of each isolated equilibrium.

(5') i1 = -2; + z 2 3 i2 = 2 1 - z2

Exercise 1.14 Find all equilibrium points of the system

XI = a21 - 21x2

X2 = b z ? - cz2

for all positive real values of a, b, and c, and determine the type of each equilibrium.

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I 1.3. EXERCISES

Exercise 1.15 The system

has an equilibrium point a t the origin.

(a) Linearize the system about the origin and find the type of the origin as an equilibrium point of the linear system.

(b) Find the phase portrait of the nonlinear system near the origin, and show that the portrait resembles a stable focus. Hint: Transform the equations into polar coordinates.

(c) Explain the discrepancy between the results of parts (a) and (b)

Exercise 1.16 For each of the followingsystems, construct the phase portrait using the isocline method and discuss the qualitative behavior of the system. You can use information about the equilibrium points or the vector field, but do not use a computer program to generate the phase portrait.

(1) XI = 2 2 cos Z]

2 2 = sin21

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54 CHAPTER 1. INTRODIICTION

Exercise 1.17 For each of the following systems, construct the phase portrait (preferably using a computer program) and discuss the qualitative behavior of the system.

(1) 21 = 2 2

22 = XI - 2 tan-' (z l + z2)

Exercise 1.18 Consider the system

( a ) Find all equilibrium points and determine the type of each point.

( b ) Construct the phase portrait, preferably using a computer program, and discuss the qualitative behavior of the system.

Exercise 1.19 Consider the tunnel-diode circuit of Section 1.1.2 with the numer- ical data used in Example 1.2, except for R and E which are taken as E = 0.2V and R = 0.2kQ.

(a) Find all equilibrium points and determine the type of each point

( b ) Construct the phase portrait, preferably using a computer program, and discuss the qualitative behavior of the circuit.

Exercise 1.20 Repeat the previous problem with E = 0.4V and R = 0.2kn.

Exercise 1.21 Consider the Hopfield neural network model of Section 1.1.5 with n = 2 , V ~ = l , a u d T z ~ = T ~ z = l . F o r i = 1 , 2 , t a k e I i = O , C i = l , p i = 1 , T,i = 0, and gi(u) = (2/a) tan-'(X?ru/2).

(a) Find all equilibrium points and determine the type of each point

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1.3. EXERCISES 55

(b ) Take X = 5. Construct the phase portrait, preferably using a computer pro- gram, and discuss the qualitative behavior of the system.

Exercise 1.22 The phase portraits of the following four systems are shown in Figures 1.37: parts (a), (b), (c), and (d), respectively. Mark the arrowheads and discuss the qualitative behavior of each system.

(4) 2 1 = 2 2

2 2 = -22 -+(XI -52)

where +(y) = y3 + 0.5y if lyl 5 1 and +(y) = 2y - 0.5 sign(y) if lyl > 1

Exercise 1.23 An equivalent circuit of the Wien-Bridge oscillator is shown in Fig- ure 1.38 [34], where g(v) is a nonlinear voltage-controlled voltage source.

(a) With X I = vcl and 5 2 = v c 2 = v as the state variables, show that the state equation is

( b ) Let C1 = C2 = R1 = R2 = 1 and g(v) = 3.234~-2.195v3+0.666v5. Construct the phase portrait, preferably using a computer program, and discuss the qualitative behavior of the system.

Exercise 1.24 Consider the mass-spring system with dry friction

j; + ky + cj , + ~ ( y , C) = 0

where 7 is defined in Section 1.1.3. Use piecewise linear analysis to construct the phase portrait qualitatively (without numerical data), and discuss the qualitative behavior of the system.

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56 CHAPTER 1. INTRODUCTION

Figure 1.37: Exercise 1.22.

Figure 1.38: Exercise 1.23.

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Chapter 2

Fundament a1 Properties

This chapter starts by recalling a few elements of mathematical analysis which will he used throughout the book. We then consider some fundamental properties of the solutions of ordinary differential equations, like existence, uniqueness, continuous dependence on initial conditions, and continuous dependence on parameters. These properties are essential for the state equation 3 = f ( t , 2) to be a useful mathematical model of a physical system. In experimenting with a physical system such as the pendulum, we expect that starting the experiment from a given initial state at time to, the system will move and its state will be defined in the (at least immediate) future time 1 > to . Moreover, with a deterministic system, we expect that if we could repeat the experiment exactly, we would get exactly the same motion and the same state at 1 > to. For the mathematical model to predict the future state of the system from its current state at to, the initial value problem

must have a unique solution. This is the question of existence and uniqueness that is addressed in Section 2.2. It is shown that existence and uniqueness can be ensured by imposing some constraints on the right-hand side function f(1, I). The key constraint used in Section 2.2 is the Lipschitz condition, whereby f(t, 2)

satisfies the inequality

for all ( t ,z ) and ( t , y) in some neighborhood of (to,zo). An essential factor in the validity of any mathematical model is the continuous

dependence of its solutions on the data of the problem. The least we should expect from a mathematical model is that arbitrarily small errors in the data will not result in large errors in the solutions obtained by the model. The data of the initial value

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58 CHAPTER 2. FUNDAMENTAL PROPERTIES

problem (2.1) are the initial state xo, the initial time to, and the right-hand side function f( t , 2). Continuous dependence on the initial conditions ( lo , zo) and on the parameters o f f are studied in Section 2.3. I f f is differentiable with respect t o its parameters, then the solution will be differentiable with respect to these parameters. This is shown in Section 2.4 and is used to derive sensitivity equations which describe the effect of small parameter variations on the performance of the system. The continuity and differentiability results of Sections 2.3 and 2.4 are valid only on finite (compact) time intervals. Continuity results on the infinite-time interval will be given later, after stability concepts have been introduced.'

The chapter ends with a brief statement of a comparison principle that bounds the solution of a scalar differential inequality 6 5 f( t , u) by the solution of the differential equation u = f ( t , u).

2.1 Mathematical Preliminaries

2.1.1 Euclidean Space

The set of all n-dimensional vectors z = (XI,. . ., z,)~, where z,, . . . ,z, are real numbers, defines the n-dimensional Euclidean space denoted by Rn. The one- dimensional Euclidean space consists of all real numbers and is denoted by R. Vectors in R" can be added by adding their corresponding components. They can be multiplied by a scalar by multiplying each component by the scalar. The inner product of two vectors x and y is xTy = CYzl z,y,.

Vector and Matrix Norms

The norm I(z(l of a vector x is a real-valued function with the propert~es

JlzJl 2 0 for all x E Rn, with 11x11 = 0 if and only if x = 0.

llx + yll 5 lIzl1+ Ilyll, for all 2, Y E Rn

IJaxlJ = JaJ llzll, for all a 6 R and z 6 Rn.

The second property is the triangle inequality. We shall consider the class of p norms, defined by

and

Il~llm = m,ax 1z.l

'See, in particular, Section 5.5.

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2.1. MATHEMATICAL PRELIMINARIES 59

The three most commonly used norms are IJzJJ1, JJxl),, and the Euclidean norm

All pnorms are equivalent in the sense that if 1 ) . 11, and ) I . JJp are two different pnorms, then there exist positive constants cl and c2 such that

for all x 6 Rn. Exercise 2.1 gives these constants for the most popular norms. A classic result concerning pnorms is the Holder inequality

for all x E Rn, y E Rn. Quite often when we use norms, we only use properties deduced from the three basic ~ r o ~ e r t i e s satisfied by any norm. In those cases, the subscript p is dropped, indicating that the norm can be any pnorm.

An m x n matrix A of real elements defines a linear mapping y = Ax from Rn into Rm. The induced pnorm of A is defined by2

which for p = 1,2, cc is given by

Xm.,(ATA) is the maximum eigenvalue of ATA. Some useful properties of induced matrix norms are summarized in Exercise 2.2.

Topological Concepts i n R"

Convergence of Sequences: A sequence of vectors xo, X I , . . ., x k , . . . in Rn, denoted by {zt), is said to converge to a limit vector x if

llxr - xll -t 0 as k -t co

which is equivalent to saying that, given any r > 0, there is N such that

I [ x ~ - ~ ( ( < c , V k z N

lsup denotes supremum, the least upper hound; inf denotes infimum, the geatest lower hound.

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60 CHAPTER 2. FUNDAMENTAL PROPERTIES

The symbol 'Y' reads "for all." A vector z is an accumulation point of a sequence { z r ] if there is a subsequence of {xt) that converges t o z; that is, if there is an infinite subset Ii of the nonnegative integers such that { z a } t e K converges to x. A bounded sequence {zt) in Rn has a t least one accumulation point in Rm. A sequence of real numbers {rt} is said to be increasing (monotonically increasing or nondecreasing) if ra < rt+l V k. If rt < r t + l , it is said to be strictly increas- ing. Decreasing (monotonically decreasing or nonincreasing) and strictly decreasing sequences are defined similarly with rt _> r t+ l . An increasing sequence of real num- bers that is bounded from above converges to a real number. Similarly, a decreasing sequence of real numbers that is bounded from below converges to a real number.

Sets : A subset S C R" is said to be open if, for every vector z E S, one can find an €-neighborhood of z

N(z, r ) = { z E R" ( (It - 21) < c )

such that N(x , r ) C S. A set S is closed if and only if its complement in R" is open. Equivalently, S is closed if and only if every convergent sequence {zk) with elements in S converges to a point in S. A set S is bounded if there is r > 0 such that l(zJJ 5 r for all z E S. A set S is compact if it is closed and bounded. A point p is a boundary point of a set S if every neighborhood of p contains a t least one point of S and one point not belonging to S. The set of all boundary points of S, denoted by aS, is called the boundary of S. A closed set contains all its boundary points. An open set contains none of its boundary points. The interior of a set S is S - as. An open set is equal t o its interior. The closure of a set S , denoted by 3, is the union of S and its boundary. A closed set is equal to its closure. An open set S is connected if every pair of points in S can be joined by an arc lying in S. A set S is called a region if it is the union of an open connected set with some, none, or all of its boundary points. If none of the boundary points are included, the region is called an open region or domain. A set S is convez if, for every z, y E S and every real number 6, 0 < 0 < 1, the point Oz + (1 - 6)y E S. If 3: E X c R" and y E Y C Rm, we say that (I, y) belongs to the product set X x Y C R" x Rm.

Con t inuous Funct ions: A function f mapping a set SI into a set Sz is denoted by f : S1 - S2. A function f : Rn -t Rm is said to be continuous a t a point x if f (zr) - f (2) whenever x r --t x . Equivalently, f is continuous a t z if, given c > 0, there is 6 > 0 such that

The symbol "+" reads "implies." A function f is continuous on a set S if i t is continuous at every point of S, and it is uniformly continuous on S if, given r > 0 there is 6 > 0 (dependent only on c ) such that the inequality holds for all z, y E S.

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2.1. MATHEMATICAL PRELIMINARIES 61

Note that uniform continuity is defined on a set, while continuity is defined at a point. For uniform continuity, the same constant 6 works for all points in the set. Clearly, i f f is uniformly continuous on a set S , then it is continuous on S . The opposite statement is not true in general. However, if S is a compact set, then continuity and uniform continuity on S are equivalent. The function

is continuous for any two scalars 01 and a2 and any two continuous functions fl and f2. If SI, S2, and S3 are any sets and fi : Sl + Sz and f2 : S 2 + S3 are functions, then the function fz o f l : S1 --t S3, defined by

is called the composition of fi and f 2 . The composition of two continuous functions is continuous. If S C Rn and f : S -r Rm, then the set of f (x) such that x E S is called the image of S under f and is denoted by f(S) . I f f is a continuous function defined on a compact set S , then f(S) is compact; hence, continuous functions on compact sets are bounded. Moreover, i f f is real-valued, that is, f : S + R, then there are points p and q in the compact set S such that f (x) < f(p) and f(x) 2 f(q) for all x E S . I f f is a continuous function defined on a connected set S, then f (S) is connected. A function f defined on a set S is said to be one-to-one on S if whenever x, y E S and x # y, then f(x) # f(y). I f f : S + Rm is a continuous, one-to-one function on a compact set S C Rn, then f has a continuous inverse f-' on f(S). The composition o f f and f-' is identity; that is, f-'(f(x)) = x. A function f : R + Rn is said to be piecewise continuous on an interval J C R if for every bounded subinterval J o c J, f is continuous for all x E Jo except, possibly, a t a finite number of points where f may have discontinuities. Moreover, a t each point of discontinuity xo, the right-side limit lim,,,o f(xo + h) and the left-side limit limb-o f(xo - h) exist; that is, the function has a finite jump a t zo. Examples of piecewise continuous functions are given in Exercise 2.4.

Differentiable funct ions: A function f : R --r R is said to be differentiable a t x if the limit

fi(x) = lim f ( x + h) - f ( x ) h-0 h

exists. The limit f'(x) is called the derivative o f f a t x. A function f : Rn -+ Rm is said to be continuously dafferentiable a t a point 2.0 if the partial derivatives afi/axj exist and are continuous at xo for 1 < i < m, 1 < j 5 n. A function f is continuously differentiable on a set S if i t is continuously differentiable a t every point of S . For a continuously differentiable function f : R" + R, the row vector a f l a x is defined

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62 CHAPTER 2. FUNDAMENTAL PROPERTIES

The gradient vector, denoted by V f ( z ) , is

For a continuously differentiable function f : R" -+ Rm, the Jacobian matrix [a f / a z ] is an m x n matrix whose element in the ith row and j th column is af i /az j . Suppose S C Rn is open, f maps S into Rm, f is continuously differentiable a t zo E S , g maps an open set containing f ( S ) into Rk, and g is continuously differ- entiable a t f(z0). Then the mapping h of S into Rk , defined by h ( z ) = g ( f ( z ) ) , is continuously differentiable a t zo and its Jacobian matrix is given by the chain rule

2.1.2 Mean Value and Implicit Function Theorems

If z and y are two distinct points in Rn, then the line segment L(z , y) joining z and y is

Mean Value Theorem

Assume that f : R" -+ R is continuously differentiable a t each point z of an open set S C Rn. Let z and y be two points of S such that the line segment L(z , y) C S. Then there exists a point z of L(z , y ) such that

Implicit Function Theorem

Assume that f : Rn x Rm + Rn is continuously differentiable a t each point ( z , y) of an open set S c Rn x Rm. Let (lo, Y o ) he a point in S for which f(z0, yo) = 0 and for which the Jacobian matrix [af /az](zo, yo) is nonsingular. Then there exist neighborhoods U C Rn of zo and V C Rm of yo such that for each y E V the equation f ( z , y) = 0 has a unique solution z E U . Moreover, this solnt~on can be given as z = g(y) where g is continuously differentiable a t y = yo.

The proof of these two theorems, as well as the other facts stated earlier in this section, can be found in any textbook on advanced calculus or mathematical analysis?

3See, for example, [q.

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2.1. MATHEMATICAL PRELIMINARIES 63

2.1.3 Gronwall-Bellman Inequality

Lemma 2.1 Let X : [a, b] + R be continuous and p : [a, b] + R be continuous and nonnegative. If a continuous function y : [a, b] + R satisfies

t

~ ( t ) 5 X(t) + P ( S ) Y ( S ) ds

for a < t < b, then on the same interval

In particular, if X(t) z X is a constant, then

If, an addition, p ( t ) s p 2 0 is a constant, then

y( t ) < exp[p(t - all

Proof: Let

z ( t ) = !J(s)v(s) ds

and v( t ) = z ( t ) + X(t) - y(t) 2 0

Then, z is differentiable and

= jl(t)y(t) = j l( t)z(t) + jl(tlX(t) - jl(t)v(t)

This is a scalar linear state equation with the state transition function

Since z (a) = 0 , we have

The term ..t

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64 CHAPTER 2. FUNDAMENTAL PROPERTIES

is nonnegative. Therefore,

Since ~ ( t ) < A(t) + t ( t ) , this completes the proof in the general case. In the special case when A(t) A , we have

= - {exp [ l P ( T ) d T ] ] l ' = t

which proves the lemma when A is a constant. The proof when both A and p are constants follows by integration. 0

2.1.4 Contraction Mapping

Consider an equation of the form z = T(z). A solution z* to this equation is said to be a fixed point of the mapping T since T leaves z* invariant. A classical idea for finding a fixed point is the successive approximation method. We begin with an initial trial vector xl and compute z2 = T(zl). Continuing in this manner it- eratively, we compute successive vectors zb+l = T(zr). The contraction mapping theorem gives sufficient conditions under which there is a fixed point z* of z = T(z) and the sequence {z*} converges to z'. It is a powerful analysis tool for proving the existence of a solution of an equation of the form x = T(z). The theorem is valid, not only when T is a mapping from one Euclidean space into another, but also when T is a mapping between Banach spaces. We shall use the contraction mapping theorem in that general setting. We start by introducing Banach spaces4

Vector Spaces: A linear vector space X over the field R 1s a set of elements z, y, r , . . . called vectors such that for any two vectors x , y E X, the sum x + y is defined, z + y E X, z + y = y + I , (z + y) + z = z + (y + z), and there is a zero vector 0 E X such that x + 0 = z for all z E X. Also for any numbers a , P E R, the scalar multiplication az is defined, ax E X, 1.2: = z, 0 . z = 0, (ap)z = ~ ( P x ) , a(z + Y) = az + ay, and (a + p)x = az + Px, for all x, y E X.

'For a complete treatment of Banach spaces, consult any textbook on functional analysis. A lucid treatment can be found in [106, Chapter 21.

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2.1. MATHEMATICAL PRELIMINARIES 65

Normed Linear Space: A linear space X is a normed linear space if, to each vector x X , there is a real-valued norm JJxJI which satisfies

11x11 > 0 for a11 z 6 X , with llzll = 0 if and only if z = 0

. IIaxII = ICY[ IIzII for all a E R and x 6 X .

If it is not clear from the context whether 11 . 11 is a norm on X or a norm on Rn, we shall write ( 1 . 112 for the norm on X .

Convergence: A sequence {zk} E X, a normed linear space, converges to z ~ X i f

11zk - 111 --+ 0 as k - oo Closed Set: A set S C X is closed if and only if every convergent sequence

with elements in S has its limit in S. Cauchy Sequence: A sequence {xk} E X is said to be a Cauchy sequence if

Every convergent sequence is Cauchy, but not vice versa

Banach Space: A normed linear space X is complete if every Cauchy sequence in X converges to a vector in X. A complete normed linear space is a Banach space.

Example 2.1 Consider the set of all continuous functions f : [a, b] + Rn, denoted by C[a, b] . This set forms a vector space on R. The sum z + y is defined by (z + y)(t) = z(t) + y(t). The scalar multiplication is defined by (az)(t) = az( t ) . The zero vector is the function identically zero on [a, b] . We define a norm by

where the right-hand side norm is any pnorm on Rn. Clearly ilzllc 2 0 and is zero only for the function which is identically zero. The triangle inequality follows from

Also maxllaz(t)ll = m=lal Ilx(t)ll = lalmaxllz(t)ll

where all maxima are taken over [a, b] . Hence, C[a, b] together with the norm (1. I ( c is a normed linear space. It is also a Banach space. To prove this claim, we need to show that every Cauchy sequence in C[a, b] converges to a vector in C[a, b] . Suppose that {zt} is a Cauchy sequence in C[a, b ] . For each fixed t E [a, b] ,

Ilxa(t) - z,(t)ll I I(zk - zm(lc + 0 as t , rn + oo

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66 CHAPTER 2. FUNDAMENTAL PROPERTIES

So { x t ( t ) ) is a Cauchy sequence in Rn. But Rn with any pno rm is complete because convergence implies componentwise convergence and R is complete. Therefore, there is a real vector z ( t ) to which the sequence converges: x t ( t ) -+ x( t ) . This proves pointwise convergence. We prove next that the convergence is uniform in t E [a,b]. Given r > 0, choose N such that J J z t - x,(lc < €12 for k , m > N . Then for k > N

I l ~ k ( t ) - 4 t ) l l 5 Ilzk(t) - ~ m ( t ) l l + 112m(t) - z(t)ll

i Ilzs - xmllc + Ilzm(t) - x(t)ll

By choosing m sufficiently large (which may depend on t ) , each term on the right- hand side can be made smaller than r/2; so Jlzk(t) - z(t)JI < r for k > N. Hence { z a ) converges to z , uniformly in t E [a, b]. To complete the proof, we need to show that z ( l ) is continuous and { z k ) converges to x in the norm of C[a, b]. To prove continuity, consider

Il4t + 6) - x(t)ll i Il4t + 6) - ~ k ( t + 6)ll

+ I l~k ( t + 6) - ~ k ( t ) l l + ll.k(t) - z(t)ll

Since { x r ) converges uniformly to x , given any r > 0, we can choose k large enough to make both the first and third terms on the right-hand side less than r/3. Since xr( t ) is continuous, we can choose 6 small enough to make the second term less than €13. Therefore z ( t ) is continuous. The convergence of zk to z in 1 ) . Ilc is a direct consequence of the uniform convergence. A

Other examples of Banach spaces are given in exercises.

Theorem 2.1 (Contraction Mapping) Let S be a closed subset of a Banach space X and let T be a mapping that maps S into S. Suppose that

IlT(z) - T(u)l\ l PI^ - ull, 'd 2 , Y E S , 0 5 P < 1

then

There ezists a unique vector z* E S satisfying z* = T ( z ' ) .

x* can be obtained by the method o f successive approzimation starting from any arbitrary initial vector in S . 0

Proof: Select an arbitrary z l E S and define the sequence { r k ) by the formula Zk+1 = T ( z k ) . Since 7' maps S into S , zr: E S for all k > 1. The first step of the proof is to show that { z t } is Cauchy. We have

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2.2. EXISTENCE AND UNIQUENESS 67

It follows that

The right-hand side tends to zero as k - m. Hence, the seqnellce is Cauchy. Since X is a Banach space,

x ~ - + x * ~ X as k - t m

Moreover, since S is closed, x* E S. We now show that x* = T(z*). For any zk = T ( z ~ - ~ ) , we have

By choosing k large enough, the right-hand side of the inequality can be made arbitrarily small. Thus, l(z* - T(z*)[I = 0; that is, x* = T(x*). It remains to show that z* is the unique fixed point of T in S. Suppose that z* and y* are fixed points. Then,

llz* - Y * I I = lIT(z*) - T(y*)ll I pllx' - Y'II Since p < 1, we have x* = y*. 0

2.2 Existence and Uniqueness

In this section, we derive sufficient conditions for the existence and uniqueness of the solution of the initial value problem (2.1). By a solution of (2.1) over an interval [to, tl] we mean a continuous function z : [to, tl] -+ Rn such that x(t) is defined and i ( t ) = f (t , z(t)) for all t E [lo, tl]. If f (t, x) is continuous in t and z, then the solution z(t) will be continuously differentiable. We will assume that f (t, z) is continuous in z but only piecewise continuous in t , in which case a solution z(t) could only be piecewise continuously differentiable. The assumption that f ( t , z) he piecewise contin~ous in t allows us to include the case when f( t , z) depends on a time-varying input that may experience step changes with time.

A differential equation with a given initial condition might have several solutions. For example, the scalar equation

i = x ' / ~ , with z(0) = 0 (2.3)

has a solution i ( t ) = ( ~ t / 3 ) ~ / ~ . This solution is not unique, since z(t) z 0 is another solution. Noting that the right-hand side of (2.3) is continuous in z , it is clear that

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68 CHAPTER 2 . FUNDAMENTAL PROPERTIES

continuity of f ( t , z ) in its arguments is not sufficient to ensure uniqueness of the solut,ion. Extra conditions must he imposed on the function f . The question of existence of a solution is less stringent. In fact, continuity of f ( t , z ) in its arguments ensures that there is at least one solution. We shall not prove this fact here.5 Instead, we prove an easier theorem that employs the Lipschitz condition to show existence and uniqueness.

T h e o r e m 2.2 (Local Existence a n d Uniqueness) Let f ( t , z ) be piecewise con- tinuous i n t and satisfy the Lipschitz condition

V I, y E B = { z E R" 1 )1z - Z O ] ~ _< r ) , V t E [ to , t l ] . Then, there ezists some 6 > 0 such that the state equation

x = f ( t , z ) , with z ( t o ) = z o

has a unique solution over [ to , to + 61. 0

Proof: We start by noting that if z ( t ) is a solution of

then, by integration, we have

Conversely, if z ( t ) satisfies ( 2 . 5 ) , then z ( t ) satisfies ( 2 . 4 ) . Thus, the study of exis- tence and uniqueness of the solution of the differential equation ( 2 . 4 ) is equivalent to the study of existence and uniqueness of the solution of the integral equation ( 2 . 5 ) . We proceed with ( 2 . 5 ) . Viewing the right-hand side of ( 2 . 5 ) as a mapping of the continuous function x : [ t o , t l ] + R", and denoting it by ( P z ) ( t ) , we can rewrite ( 2 . 5 ) as

z ( t ) = ( P z ) ( t ) ( 2 .6 )

Note that ( P z ) ( t ) is contiuuous in 1 . A solution of ( 2 . 6 ) is a fixed point of the map- ping P that, maps z into P x . Existence of a fixed point of (2.6) can be established using the contraction mapping theorem. This requires defining a Banach space X and a closed set S c X such that P maps S into S and is a contraction over S. Let

X = C [ t o , to + 61, with norm (Iz(lc = maw ( I x ( t ) ( ( t€[t . , t~+sl

'See [118, Theorem 2.31 for a proof.

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2.2. EXISTENCE AND UNIQUENESS 69

and S = {z E X 1 llx - xollc 5 7 )

where T is the radius of the ball B and 6 is a positive constant to be chosen. We shall restrict the choice of 6 to satisfy 6 5 t l -to, so that [to, to+6] C [to, tl]. Notice that [lx(t)ll denotes a norm on R", while llxllc denotes a norm on X. Also, B is a ball in Rn while S is a ball in X. By definition, P maps X into X. To show that it maps S into S , write

By piecewise continuity o f f , we know that f ( t , zo) is bounded on [to, tl]. Let

Using the Lipschitz condition (2.2) and the fact that for each x E S ,

we obtain

and IJPz - xollc = max )I(Pz)(t) - xoll 5 6(Lr + h)

t ~ [ ~ , . t 0 + s i

Hence, choosing 6 5 ~ / ( L T + h) ensures that P maps S into S. To show that P is a contraction mapping over S , let x and y E S and consider

I: Ilf(s, ~ ( 8 ) ) - f ( s , y(s))ll d s

t t Lo s - Y(S)II d s 5 d s L I Z - vllc t o

Therefore,

P ( ( P x - P y ( l c I LJIlz - yllc I pllz - yllc for 6 5 j;

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70 CHAPTER 2. FUNDAMENTAL PROPERTIES

Thus, choosing p < 1 and 6 < p/L ensures that P is a contraction mapping over S. By the contraction mapping theorem, we can conclude that if 6 is chosen to satisfy

then (2.5) will have a unique solution in S. This is not the end of the proof, though, since we are interested in establishing uniqueness of the solution among all continuous functions x(t), that is, uniqueness in X. It turns out that any solution of (2.5) in X will lie in S. To see this, note that since +(to) = xo is inside the ball B, any continuous solution z(t) must lie inside B for some interval of time. Suppose that z(t) leaves the hall B, and let to + p be the first t,in~e z(t) intersects the boundary of B. Then,

Ilz(to + P) - "011 = r On the other hand, for all t < to + p ,

Therefore,

Hence, the solution x(t) cannot leave the set B within the time interval [to, t o + 61, which implies that any solution in X lies in S. Consequently, uniqueness of the solution in S implies uniqueness in X. 0

The key assumption in Theorem 2.2 is the Lipschitz condition (2.2). A function satisfying (2.2) is said to he Lipschitz in x, and the positive constant L is called a Lipschitz constant. We also use the words locally Lipschitz and globally Lipschitz to indicate the domain over which the Lipschitz condition holds. Let us introduce the terminology first for the case when f depends only on x. A function f(x) is said to be locally Lipschitz on a domain (open and connected set) D C Rn if each point of D has a neighborhood Do such that f satisfies the Lipschitz condition (2.2) for all points in Do with some Lipschitz constant Lo. We say that f is Lipschitz on a set W if it satisfies (2.2) for all points in W, with the same Lipschitz constant L. A locally Lipschitz function on a domain D is not necessarily Lipschitz on D, since the Lipschitz condition may not hold uniformly (with the same constant L) for all points in D. However, a locally Lipschitz function on a domain D is Lipschitz on every compact (closed and bounded) subset of D (Exercise 2.16). A function f(x)

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is said to be globally Lipschitt if it is Lipschitz on Rn. The same terminology is extended to a function f ( t , z ) , provided the Lipschitz condition holds uniformly in t for all t in a given interval of time. For example, f ( t , z ) is locally Lipschitz in z on [a, b] x D C R x Rn if each point z E D has a neighborhood Do such that f satisfies (2.2) on [a, b] x Do with some Lipschitz constant Lo. We shall say that f ( t , z ) is locally Lipschitz in z on [ t o , w ) x D if it is locally Lipschitz in x on [a, b] x D for every compact interval [a, b] C [to, w ) . A function f ( t , x ) is Lipschitz in z on [a, b] x W if it satisfies (2.2) for all t E [a, b] and all points in W , with the same Lipschitz constant L.

When f : R + R, the Lipschitz condition can be written as

which implies that on a plot of f ( x ) versus z , a straight line joining any two points of f ( z ) cannot have a slope whose absolute value is greater than L. Therefore, any function f ( z ) that has infinite slope at some point is not locally Lipschitz at that point. For example, any discontinuous function is not locally Lipschitz at the point of discontinuity. As another example, the function f ( x ) = +'I3, which was used in (2.3), is not locally Lipschitz at z = 0 since f l ( z ) = 5z-2 /3 + w as 2 + 0. On the other hand, if 1 f '(z)l is bounded by a constant k over the interval of interest, then f ( z ) is Lipschitz on the same interval with Lipschitz constant L = k. This observation extends to vector-valued functions, as demonstrated by the following lemma.

Lemma 2.2 Let f : [a,b] x D + Rm be continuous for some domain D c Rn. Suppose [ a f / a z ] exists and is continuous on [a , b] x D. If, for a convex subset W C D, there is a constant L 2 0 such that

on [a, b] x W , then

Ilf(t> 2 ) - f(t3y)ll < L112 - yll f o r a l l t € [ a , b ] , z E W , a n d y e w .

Proof: Let II.II, be the underlying norm for any p 6 [ I , w], and determine q E [I , w] from the relationship l / p + 1/q = 1 . Fix t E [a, b], z E W , and y E W. Define y(s ) = (1 - s ) z + sy for all s E R such that y(s) E D. Since W c D is convex, y(s ) E W for 0 < s < 1. Take z E Rm such that6

'Such 2 always exists; see Exercise 2.19.

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72 CHAPTER 2. FUNDAMENTAL PROPERTIES

Set g(s) = zT f(1, y(s)). Since g(s) is a real-valued function which is continuously differentiable in an open interval that includes [0, 11, we conclude by the mean value theorem that there is s l E ( 0 , l ) such that

Evaluating g at s = 0, s = 1, and calculating gl(s) using the chain rule, we obtain

where we used the Holder inequality lzTwl 5 IIzllqllwIlp.

The proof of the lemmashows how a Lipschitz constant can be calculated using knowledge of [a f l ax] .

The Lipschitz property of a function is stronger than continuity. It can be easily seen that if f (z ) is Lipschitz on W, then it is uniformly continuous on W (Exercise 2.17). The converse is not true, as seen from the function f (z ) = z1I3, which is continuous but not locally Lipschitz a t z = 0. The Lipschitz property is weaker than continuous differentiability, as stated in the following lemma.

Lemma 2.3 Let f ( t , z ) be continuous on [a, b] x D, for some domain D c R". If [af/az] exists and is continuous on [a, b] x D, then f is locally Lipschitz in z on [a,b] x D. 0

Proof: For zo E D , let r be so small that the ball Do = {z E Rn I llz - zoll 5 r) is contained in D. The set Do is convex and compact. By continuity, [af/az] is bounded on [a, b] x D . Let Lo be a bound for llaf/azll on [a, b] x Do. By Lemma2.2, f is Lipschitz on [a, b] x Do with Lipschitz constant Lo.

It is left as an exercise to the reader (Exercise 2.20) to extend the proof of Lemma 2.2 to prove the following lemma.

Lemma 2.4 Let f (t, z ) be continuous on [a, b] x Rn. If [a f /ax] exists and is con- tinuous on [a, b] x Rn, then f is globally Lipschilz in z on [a, b] x Rn if and only if [af/az] is uniformly bounded on [a, b] x Rn. 0

Example 2.2 The function

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2.2. EXISTENCE AND UNIQUENESS 73

is continuously differentiable on R2. Hence, it is locally Lipschitz on R2. It is not globally Lipschitz since [affax] is not uniformly bounded on R2. On any compact subset of R ~ , f is Lipschitz. Suppose we are interested in calculating a Lipschitz constant over the convex set

The Jacobian matrix [affax] is given by

Using (1.(1, for vectors in R2 and the induced matrix norm for matrices, we have

All points in W satisfy

Hence,

and a Lipschitz constant can be taken as L = 1 + a1 + az. Example 2.3 Consider the function

where the saturation function sat(.) is defined by

-1, for y < -1 Y, for lyl 5 1 1, f o r y > l

The function f is not continuously differentiable on R2. Let us check its Lipschitz property by examining f(x) - f(y). Using ( I . ( 1 2 for vectors in R2 and the fact that the saturation function sat(.) satisfies

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74 CHAPTER 2. FUNDAMENTAL PROPERTIES

we obtain

Using the inequality

we conclude that

Here we have used a property of positive semidefinite symmetric matrices; that is, z T p z < A,,(P) zTz, for all z E Rn, where A,,(.) is the maximumeigenvalue of the matrix. A more conservative (larger) Lipschitz constant will be obtained if we use the more conservative inequality

resulting in a Lipschitz constant L = &. A

In these two examples, we have used (1 . (I, in one case and (1 . ( ( 2 in the other. Due to equivalence of norms, the choice of a norm on Rn does not affect the Lip- schitz property of a function. I t only affects the value of the Lipschitz constant (Exercise 2.21). Example 2.3 illustrates the fact that the Lipschitz condition (2.2) does not uniquely define the Lipschitz constant L. If (2.2) is satisfied with some positive constant L, i t is satisfied with any positive constant larger than L. This nonuniqueuess can be removed by defining L to be the smallest constant for which (2.2) is satisfied, but we seldom need to do that.

Theorem 2.2 is a local theorem since it guarantees existence and uniqueness only over an interval [to, to + 61, where 6 may be very small. In other words, we have no control on 6; hence, we cannot ensure existence and uniqueness over a given time interval [to, tr]. However, one may try to extend the interval of existence by repeated applications of the local theorem. Starting at a time to with an initial state x(t0) = zo, Theorem 2.2 shows that there is a positive constant 6 (dependent on zo) such that the state equation(2.1) has a unique solution over the time interval [to, to + 61. Now, taking to + 6 as a new initial time and z(to + 6) as a new initial state, one may try to apply Theorem 2.2 to establish existence of the solution beyond to+6. If all the conditions of the theorem are satisfied a t [to+&, z(to+6)], then there exists 62 > 0 such that the equation has a unique solution over [to + 6, to + 6 + that passes through the point [to+6, z(to+6)]. We piece together the solutions over

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2.2. EXISTENCE AND UNIQUENESS 75

[ to , to + 61 and [to + 6 , to + 6 + 621 to establish the existence of a unique solution over [ to , lo + 6 + 621. This idea can be repeated to keep extending the solution. However, in general, the interval of existence of the solution cannot be extended indefinitely because the conditions of Theorem 2.2 may cease to hold. There is a maximum interval [ t o , T ) where the unique solution starting at ( t 0 , x o ) exists.' In general, T may be less than t ~ , in which case as t -+ T , the solution leaves any compact set over which f is locally Lipschitz in x (Exercise 2.33).

Example 2.4 Consider the scalar system

2: = - x 2 , with x ( 0 ) = -1

The function f ( x ) = - x 2 is locally Lipschitz for all x E R. Hence, i t is Lipschitz on any compact subset of R. The unique solution

exists over [O, 1). As t -+ 1, x ( t ) leaves any compact set. A

The phrase "finite escape time" is used to describe the phenomenon that a trajectory escapes to infinity a t a finite time. In Example 2.4, we say that the trajectory has a finite escape time at t = 1.

In view of the discussion preceding Example 2.4, one may pose the question: When is i t guaranteed that the solution can be extended indefinitely? One way to answer this question is to require additional conditions which ensure that the solution x ( t ) will always be in a set where f ( t , x ) is uniformly Lipschitz in x . This is done in the next theorem by requiring f to satisfy a global Lipschitz condition. The theorem establishes the existence of a unique solution over [to, t l ] where t , may be arbitrarily large.

T h e o r e m 2.3 (Globa l Exis tence and Uniqueness) Suppose f ( t , x ) i s piecewise continuous i n t and satisfies

V Z, y E Rn, V t E [ to , t l ] . Then, the state equation

x = f ( t , x ) , with x ( t o ) = x o

has a unique solution over [ to , t l ] .

'For a proof of this statement, see [70, Section 8.5) or [118, Section 2.31.

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76 CHAPTER 2. FUNDAMENTAL PROPERTIES

Proof: The key point of the proof is to show that the constant 6 of Theorem 2.2 can be made independent of the initial state 20. From (2.7), we see that the dependence of 6 on the initial state comes through the constant h in the term r/(Lr + h). Since in the current case the Lipschitz condition holds globally, we can choose r arbitrarily large. Therefore, for any finite h, we can choose r large enough so that r/(Lr + h) > p/L. This reduces (2.7) to the requirement

If 11 - t o 5 p/L, we could choose 6 = t l - t o and be done. Otherwise, we choose 6 to satisfy 6 < p/L. Now, divide [to, tl] into a finite number of subintervals of length 6 < p/L, and apply Theorem 2.2 repeatedly.' 0

Example 2.5 Consider the linear system

where A(.) and g(.) are piecewise continuous functions o f t . Over any finite interval of time [to, tl], the elements of A(t) and g(t) are bounded. Hence, IIA(t)ll < a and 11g(t)ll < 6 , where llgll canbe any norm on Rn and IlAll is the induced matrix norm. The conditions of Theorem 2.3 are satisfied since

and

Ilf(t,xo)ll = IIA(t).o + s(t)ll < allzoll + b < h, for each finite 2 0 , V t E [to,tl]

Therefore, Theorem 2.3 shows that the linear system has a unique solution over [to, tl]. Since t l can he arbitrarily large, we can also conclude that if A(t) and g(t) are piecewise continuous V t 2 to , then the system has a unique solution V t 2 l o . Therefore, the system cannot have a finite escape time. A

For the linear system of Example 2.5, the global Lipschitz condition of Theorem 2.3 is a reasonable requirement. This may not be the case for nonlinear systems, in general. We should distinguish between the local Lipschitz requirement of Theorem 2.2 and the global Lipschitz requirement of Theorem 2.3. Local Lipschitz property of a function is basically a smoothness requirement. I t is implied by continuous

8Note that the initial state of each subinterval rl, say, will satisfy [lf(t,zl)ll 5 hl for some finite hl .

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2.2. EXISTENCE AND UNIQUENESS 77

differentiability. Except for discontinuous nonlinearities, which are idealizations of physical phenomena, it is reasonable to expect models of physical systems to have locally Lipschitz right-hand side functions. Examples of continuous functions which are not locally Lipschitz are quite exceptional and rarely arise in practice. The global Lipschitz property, on the other hand, is restrictive. Models of many physical systems fail to satisfy it. One can easily construct smooth meaningful examples which do not have the global Lipschitz property, but do have unique global solutions, which is an indication of the conservative nature of Theorem 2.3.

Example 2.6 Consider the scalar system

The function f(z) does not satisfy a global Lipschitz condition since the Jacobian a f / a x = -3x2 is not globally bounded. Nevertheless, for any initial state x( to ) = xo, the equation has the unique solution

x ( t ) = sign(xo) 1 + 2 x 3 1 - to )

which is well defined for all t 2 to . A

In view of the conservative nature of the global Lipschitz condition, it would be useful to have a global existence and uniqueness theorem that requires the function f to be only locally Lipschitz. The following theorem achieves that at the expense of having to know more about the solution of the system.

Theorem 2.4 Let f ( t , x ) be piecewise continuous i n t and locally Lipschitz in x for all t 2 t o and all x in a domain D C R". Let W be a compact subset of D, xo E W , and suppose it is known that every solution of

a = f ( t , x ) , .(to) = xo

lies entirely i n W . Then, there i s a unique solution that i s defined for all t 2 t o . 0

Proof: Recall the discussion on extending solutions, preceding Example 2 . 4 . By Theorem 2.2, there is a unique local solution over [ to , t o + 6 ] . Let [ t o , T ) be its max- imal interval of existence. We want to show that T = ca. Recall (Exercise 2.33) the fact that if T is finite, then the solution must leave any compact subset of D. Since the solution never leaves the compact set W, we conclude that T = ca. 0

The trick in applying Theorem 2.4 is in checking the assumption that every solution lies in a compact set without actually solving the differential equation. We shall see in Chapter 3 that Lyapunov's method for studying stability is very valuable in that regard. For now, let us illustrate the application of the theorem by a simple example.

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78 CHAPTER 2. FUNDAMENTAL PROPERTIES

Example 2.7 Consider again the system

of Example 2.6. The function f(z) is locally Lipschitz on R. If, a t any instant of time, x(t) is positive, the derivative x(t) will be negative. Similarly, if x(t) is negative, the derivative x(t) will be positive. Therefore, starting from any initial condition x(0) = a, the solution cannot leave the compact set {x E R I 1x1 5 ( a ( } . Thus, without calculating the solution, we conclude by Theorem 2.4 that the equation has a unique solution for all t 2 0. A

2.3 Continuous Dependence on Initial Conditions and Parameters

For the solution of the state equation (2.1) to be of any interest, i t must depend continuously on the initial state 20, the initial time to, and the right-hand side function f( t , x). Continuous dependence on the initial time is obvious from the integral expression (2.5). Therefore, we leave it as an exercise (Exercise 2.44) and concentrate our attention on continuous dependence on the initial state xo and the function f . Let y(t) be a solution of (2.1) that starts a t y(to) = yo and is defined on the compact time interval [to, tl]. The solution depends continuously on yo if solutions starting at nearby points are defined on the same time interval and remain close to each other in this interval. This statement can be made precise with the 6-6 argument: given r > 0, there is 6 > 0 such that for all zo in the

< ball {z E Rn I [lx - yo11 < 63, the equation 2 = f ( t , x ) has a unique solution r( t ) defined on [to, tl], with r(to) = r o , and satisfies (Ir(t) - y(t)ll < c for all t E [to, tl]. Continuous dependence on the righehand side function f is defined similarly, but to state the definition precisely we need a mathematical representation of the perturbation o f f . One possible representation is to replace f by a sequence of functions f, which converge uniformly to f as rn - m. For each function f,, the solution of x = f,(t,x) with x(to) = 20 is denoted by x,(t). The solution is said to depend continuously on the right-hand side function if z,(t) -t x(t) as m - m. This approach is a little bit involved, and will not be pursued here.g A more restrictive, but simpler, mathematical representation is to assume that f depends continuously on a set of constant parameters; that is, f = f ( t , x , X) where X E RP. The constant parameters could represent physical parameters of the , system, and the study of perturbation of these parameters accounts for modeling errors or changes in the parameter values due t o aging. Let x(t, Xo) be a solution of x = f(t,x,Xo) defined on [to, t l ] , with x(to, Xo) = xo. The solution is said to

'See (36, Section 1.31, (65, Section 1.31, or (118, Section2.51for results on continuousdependence on parametem using this approach.

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2.3. CONTINUITY OF SOLUTIONS 79

depend continuously on A if for any c > 0, there is 6 > 0 such that for all A in the ball {A E RP I IIA - A011 < 61, the equation x = f ( t , x , A ) has a unique solution x ( t , A) defined on [to, t l ] with z( to , A ) = xo, and satisfies llx(t, A) - x ( t , Ao)ll < c for all t E [to, t i ] .

Continuous dependence on initial states and continuous dependence on param- eters can be studied simultaneously. We start with a simple result which bypasses the issue of existence and uniqueness and concentrates on the closeness of solutions.

Theorem 2.5 Let f ( t , x ) be piecewise conlinuous in t and Lipschilz in z on [to, t l ] x W with a Lipschitz constant L, where W c Rn is an open connected set. Let y(t) and z ( t ) be solutions of

Lj = f ( t , Y ) , Y(t0) = YO and

i = j ( t , z ) + g ( t , z ) , 4 0 ) = zo

such that y ( t ) , z ( t ) E W for all t E [to, t l ] . Suppose that

for some p > 0 , and I I Y O -roll 5 -I

Then,

Ily(t) - z(t)ll 5 r exp[L(t - to ) ] + $ {exp[L(t - to)] - 11 Q t E [to, t l l .

Proof: The solutions y( t ) and z ( t ) are given by

Subtracting the two equations and taking norms yield

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80 CHAPTER 2. FUNDAMENTAL PROPERTIES

Application of the Gronwall-Bellman inequality to the function lly(t) - z(t)ll results in

Integrating the right-hand side by parts, we obtain

Ily(t) - z(t)ll 5 7 + p(t - to) - Y - ~ ( t - to) + Y exp[L(t - to)] t

+ lo P exp[L(t - S)I ds

I" = 7 exp[L(t - to)] + {exp[L(t -to)] - 1)

which completes the proof of the theorem.

With Theorem 2.5 in hand, we can prove the following theorem on the continu~ty of solutions in terms of initial states and parameters.

Theorem 2.6 Let f ( t ,x ,A) be continuous in (t,x,X) and locally Lipschitz in x (uniformly in t and A) on [to, tl] x D x {IIX - A011 5 c ) , where D c Rn is an open connected set. Let y(t, Ao) be a solution of i = f ( t , x, Ao) with y(to, Ao) = yo E D. Suppose y(t,Ao) is defined and belongs lo D for all t E [to,tl]. Then, given r > 0, there is 6 > 0, such that if

1\20 - yo11 < 6 and JIA - Aoll < 6

then there is a unique solution z(t, A) of i = f ( t , x , A) defined on [to,tl], with z(tO, A) = 20, and r( t , A) satisfies

Proof: By continuity of y(t, Xo) in t and the compactness of [to, t,], we know that y(l,Ao) is uniformly bounded on [to,tl]. Define a "tube" U around the solution y(t, Ao) (see Figure 2.1) by

U = {(t, x) E [to, ti1 x Rn I Ilx - ~ ( t , Xo)ll < e l

Suppose U C [to, t l] x D; if not, replace r by an r l < E that is small enough to ensure that U C [to, 111 x D and continue the proof with €1. The set U is compact; hence, f ( t , x, A) is Lipschitz in z on U with a Lipschitz constant, say, L. By continuity of f in A , for any a > 0 there is p > 0 (with p < c) such that

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2.4. DIFFERENTIABILITY OF SOLUTIONS 81

Figure 2.1: A tube constructed around the solution y(t),

Take a < r and llzo - yo11 < a. By the local existence and uniqueness theorem, there is a unique solution t ( t , A) on some time interval [to, to + A]. The solution starts inside the tube U , and as long as it remains in the tube it can he extended. We will show that, by choosing a small enough a, the solution remains in U for all t E [to, tl]. In particular, we let r he the first time the solution leaves the tube and show that we can make r > t l . On the time interval [to,r], all the conditions of Theorem 2.5 are satisfied with y = p = a. Hence,

< a 1 + - exp[L(t - to)] ( t) Choosing a 5 rLexp[-L(tl - to)]/(l+ L) ensures that the solution t(t ,A) cannot leave the tube during the interval [to, tl]. Therefore, z(t, A) is defined on [to, tl] and satisfies llz(t, A) - y(t, Ao)(( < r. Taking 6 = min{a, p} completes the proof of the theorem. 0

2.4 Differentiability of Solutions and Sensitivity Equations

Suppose f ( t , x , A) is continuous in ( t ,x , A) and has continuous first partial deriva- tives with respect to 2: and A for all (t, x , A) E [to, t l] x R" x RP. Let Ao be a nominal value of A , and suppose the nominal state equation

x = f ( t , x, Ao), with z(to) = zo

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82 CHAPTER 2. FUNDAMENTAL PROPERTIES

has a unique solution z(t, Xo) over [to, t l ] . From Theorem 2.6, we know that for all X sufficiently close to Xo, that is, IIX - Xol l sufficiently small, the state equation

x = ( t z A), with z(t0) = zo

has a unique solution z(t, A) over [to, 111 that is close to the nominalsolution z(t, Xo). The continuous differentiability o f f with respect to z and X implies the additional property that the solution z(t, A) is differentiable with respect to X near Xo. To see this, write

t

z(t. A) = 20 + / f ( s z ( s A), A) ds t o

Taking partial derivatives with respect to X yields

where Zh(t,X) = [8x(t,X)/aX] and [azo/OX] = 0, since zo is independent of A. Differentiating with respect to t, it can be seen that z ~ ( t , A) satisfies the differential equation

a - z ~ ( t , A) = A(t, X)ZA(~, A) + B(t, A), z~ ( t o , A) = 0 at (2.8)

where

A(t , A) = , B(t,X) = az s=n(*,A)

For X sufficiently close to Xo, the matrices A(t, A) and B(t, X) are defined on [to, tl]. Hence, z ~ ( t , A) is defined on the same interval. At X = Xo, the right-hand side of (2.8) depends only on the nominal solution z(t, XO). Let S(t) = z ~ ( t , Xo); then S(t) is the unique solution of the equation

The function S(t) is called the sensitivity function, and (2.9) is called the sensitivity equation. Sensitivity functions provide first-order estimates of the effect of param- eter variations on solutions. They can also be used to approximate the solution when X is sufficiently close to its nominal value Xo. For small IIX - Xol l , z(t, A) can be expanded in a Taylor series about the nominal solution z(t, Xo) to obtain

z(t, A) = z(t, An) + S(t)(X - Xo) + higher-order terms

Neglecting the higher-order terms, the solution z(t, A) can be approximated by

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2.4. DIFFERENTIABILITY O F SOLUTIONS 83

We shall not justify this approximation here. It will be justified in Chapter 7 when we study the perturbation theory. The significance of (2.10) is in the fact that knowledge of the nominal solution and the sensitivity function suffices to approxi- mate the solution for all values of X in a (small) hall centered at Xo.

The procedure for calculating the sensitivity function S(t) is summarized by the following steps:

Solve the nominal state equation for the nominal solution z(t , Xo)

Evaluate the Jacobian matrices

r Solve the sensitivity equation (2.10) for S(t)

In this procedure, we need to solve a nonlinear nominal state equation and a linear timevarying sensitivity equation. Except for some trivial cases, we will he forced t o solve these equations numerically. An alternative approach for calculating S(t) is to solve for the nominal solution and the sensitivity function simultaneously. A procedure for calculating z ~ ( t , A) is to append the variational equation (2.8) with the original state equation to obtain the (n + np) augmented equation

which is solved numerically. The sensitivity function S(t) can he calculated by solving (2.11) a t the nominal value X = Xo. Notice that if the original state equation is autonomous, that is, f ( t , z , A) = f(z , A), then the augmented equation (2.11) will be autonomous a s well. We illustrate the latter procedure by the following example.

Example 2.8 Consider the phaselocked loop equation

21 = 2 2 = f1(zt ,zz) 22 = -csinzl - ( a + bcosz1)zz = f2(z1,zz)

and suppose the parameters a , b, and c have the nominal values a0 = 1, bo = 0, and co = 1. The nominal system is given by

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84 CHAPTER 2. FUNDAMENTAL PROPERTIES

The Jacobian matrices [a f /ax] and [a f /ax] are given by I

af - [af O f 811 = [ o - 0 a x - Z ab X -z2 -zz cosz, - sin21 O I

Evaluate these Jacobian matrices a t the nominal parameters a = 1, b = 0, and c = 1 to obtain

0

To solve for S( t ) numerically, we solve (2.11) a t the nominal values of the parame- ters. Let

& 3 & 23 2 5 2 7 aa ab a~

S =

Then (2.11) is given by

221

-sin21 - 2 2 ,

2 4 r

-23 cos 21 - xq - 2 2 ,

262

-25 COS 21 - 2'6 - 2 2 cos 21,

28,

-27 cos 21 - 28 - sin 21,

The solution of this equation was computed for the initial state +lo = 2-20 = 1. Figure 2.2(a) shows 23, 25, and 27, which are the sensitivities of X I with respect to a , b, and c, respectively. Figure 2.2(h) shows the corresponding quantities for 22. Inspection of these figures shows that the solution is more sensitive to variations in the parameter c than to variations in the parameters a and b. This pattern is consistent when we solve for other initial states. A

2.5 Comparison Principle

Quite often when we study the state equation 2 = f ( t , z ) we need to compute bounds on the solution z(t) without computing the solution itself. The Gronwall- Bellman inequality (Lemma 2.1) is one tool that can be used toward that goal. An- other tool is the comparison lemma. I t applies to a situation where the derivative of

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2.4. COMPARISON PRINCIPLE 85

Figure 2.2: Sensitivity functions for Example 2.8

a scalar differentiable function v ( t ) satisfies inequality of the form v( t ) 5 f ( t , v ( t ) ) for all t in a certain time interval. Such inequality is called a differential inequality and a function v ( t ) satisfying the inequality is called a solution of the differential in- equality. The comparison lemma compares the solution of the differential inequality v ( t ) < f ( t , v ( t ) ) to the solution of the differential equation u = f ( t , u ) . The lemma applies even when v ( t ) is not differentiable, but has an upper right-hand derivative D+v(t) which satisfies a differential inequality. The upper right-hand derivative D+v(t) is defined in Appendix A.1. For our purposes, it is enough to know two facts:

if v ( t ) is differentiable at t , then D+v(t) = ~ ( t ) ;

and

then D+v(t) < go(tj

The limit h + O+ means that h approaches zero from above.

Lemma 2.5 (Comparison Lemma) Consider the scalar differential equation

where f ( t , u ) is continuous in t and locally Lipschitz in u, for all t 2 0 and all u E J C R. Let [ t o , T ) (T could be infinity) be the mazimal internal of ezistence

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86 CHAPTER 2 . FUNDAMENTAL PROPERTIES

of the solution u ( t ) , and suppose u ( t ) E J for all t E [ to , T ) . Let v ( t ) be a con- tinuous function whose upper right-hand derivative D+v(t) satisfies the differenlzal inequality

D+v(t) 5 f ( t , v ( t ) ) , .(to) < uo

with v ( t ) E J for all t E [ t o , T ) . Then, v ( t ) < u ( t ) for all t E [ t o , T ) . 0

Proof: Appendix A.1.

Example 2.9 The scalar differential equation

has a unique solution on [O,tl) for some tl > 0, because f ( z ) is locally Lipschitz. Let v( t ) = z Z ( t ) . The function v( t ) is differentiable and its derivative is given by

Hence, v ( t ) satisfies the differential inequality

Let u ( t ) be the solution of the differential equation

Then, by the comparison lemma, the solution z ( t ) is defined for all t 2 0 and satisfies

Iz(t)l = 5 e-'lal, V t 2 0

n

Example 2.10 The scalar differential equation

has a unique solution on [ O , t l ) for some tl > 0, because f ( t , z ) is locally Lipschitz in z . We want to find an upper hound on iz(t)l similar to the one we obtained in the previous example. Let us start with v ( t ) = z 2 ( t ) as in the previous example. The derivative of v is given by

We can apply the comparison lemma to this differential inequality, but the resulting differential equation will not be easy to solve. Instead, we consider a different choice

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2.4. COMPARISON PRINCIPLE 87

of v(t). Let v(t) = (x(t)l. For z( t ) # 0, the function v(t) is differentiable and its derivative is given by

Since 1 + x2(t) 2 1, we have -Iz(t)l[l+ zz(t)] 5 -(z(t)l and v(t) < -v(t) + et . On the other hand, when z(t) = 0 we have

Since f ( t , z ( t ) ) is a continuous function o f t , given any r > 0 there is 6 > 0 such that for all I T - tl < 6, i f ( r , z ( r ) ) - f ( t , x(t))l < E . Hence, for all h < 6,

which shows that t+h

h+O+

Thus, D+v(t) 5 I f(t,O)I = et whenever z( t ) = 0. Thus, for all t E [0, t l ) , we have

Letting u(t) he the solution of the linear differential equation

we conclude by the comparison lemma that

v(t) 5 u(t) = e-*lal+ 4 [e" e - 7 , V t E [O,tl)

The upper bound on v(t) is finite for every finite tl and approaches infinity only as t l + oo. Thus, the solution x(t) is defined for all t 2 0 and satisfies

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88 CHAPTER 2. FUNDAMENTAL PROPERTIES

2.6 Exercises

Exercise 2.1 Show that, for any x E Rn, we have

11~112 5 11~111 5 J;; llxllz

11~11m 5 11~112 5 J;; 11~llm

llxllm 5 11~111 5 n llxllm

Exercise 2.2 Show that, for any m x n real matrix A and any n x q real matrix B, we have

Exercise 2.3 Consider the set S = {x E R2 I - 1 < xi < 1, i = 1,2) . Is S open? Is i t closed? Find the closure, interior, and boundary of S.

Exercise 2.4 Let u ~ ( t ) be the unit step function, defined by u ~ ( t ) = 0 for t < T and u ~ ( t ) = 1 for t 2 T.

(a) Show that u ~ ( t ) is piecewise continuous.

(b) Show that f(t) = g(t)u.r(t), for any continuous function g(t), is piecewise continuous.

(c) Show that the periodic square waveform is piecewise continuous.

Exercise 2.5 Let f(x) be a continuously differentiable function that maps a convex domain D c R" into R". Suppose D contains the origin x = 0 and f(0) = 0. Show that

Hin t : Set g(u) = f(ux) for 0 < o 5 1 and use the fact that g(l)-g(0) = J: g'(o) do.

Exercise 2.6 Let f(x) be continuously differentiable. Show that an equilibrium point x* of x = f(x) is isolated if the Jacobian matrix [af/ax](x*) is nonsingular. Hin t : Use the implicit function theorem.

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2.6. EXERCISES 89

Exercise 2.7 Let y ( t ) be a nonnegative scalar function that satisfies the inequality

where k l , k 2 , k3 are nonnegative constants and a is a positive constant that satisfies a > k2. Using the Gronwall-Bellman inequality, show that

k3 y ( t ) < h e - ( a - k z ) ( t - t o ) + - - e - ( o - k . ) ( t - t o )

a - k2 1 Hint : Take z ( t ) = y(t)eu("to) and find the inequality satisfied by z .

Exercise 2.8 Let C z be the set of all piecewise continuous functions u : [0, oo) -+

R" with the property that each component is square integrable on [0, co); that is,

Jr lui(t)12 dt < oo. Define I I u I I L , = d m . Show that I J u l J r , is a well-defined norm. Hint: Use the Cauchy-Schwartz inequality

for all nonnegative scalar functions u ( t ) and ~ ( t ) .

Exercise 2.9 Let 12 be the set of all sequences of scalars { q l , q z , . . .) for which C:, l q ; l 2 < oo and define

(a) Show that llzll, is a well-defined norm

(b) Show that 12 with the norm ( ( ~ ( 1 , is a Banach space

Exercise 2.10 Let S be the set of all half-wave symmetric periodic signals of fun- damental frequency w, which have finite energy on any finite interval. A signal y E S can be represented by its Fourier series

~ ( t ) = ar exp ( jkwt ) , lar 1' < cm k add k add

Define

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90 CHAPTER 2. FUNDAMENTAL PROPERTIES

( a ) Show that IJyl(s is a well-defined norm.

(b) Show that S with the norm Ilylls is a Banach space.

Exercise 2.11 Let L, be the set of all piecewise continuous functions u : [O,w) - Rn with the property that each component ui(t) is uniformly bounded for all t 2 0. Let I I u I I L ~ = IIu(t)ll, where 1 1 . 1 1 is any pnorm.

( a ) Show that I I u ~ ~ L - is a well-defined norm.

(b ) Show that C, with the norm l)ul l~, is a Banach space.

Exercise 2.12 Consider the linear algebraic equation Ax = b, where the matrix A is n x n. Let aij denote the element of A in the ith row and j th column. Assume that aii # 0 for all i and the matrix A has the strict diagonal dominance property; that is,

laiil > laijl j 2:

Show that Ax = b has a unique solution which can be computed via the successive approximations:

D X ( ~ + ~ ) = (D - A ) x ( ~ ) + b , k 2 i where D = diag[all, azz, . . . , a,,] and x(') is any vector in Rn.

Exercise 2.13 Consider the nonlinear algebraic equation

where D is an n x n nonsingular matrix, b and c are n-vectors, and a and c > 0 are scalars. Show that, for sufficiently small r , the equation has a unique real root in the set {x E R I ((1: - D - l ~ J / Z 5 1).

Exercise 2.14 Consider the discrete-time dynamical system x(k + 1) = Ax(k).

(a) Show that x(k) -+ 0 as k -+ cc if and only if all eigenvalues of A satisfy IXiI < 1.

( b ) Can you conclude from part (a) that the eigenvalue condition ] X i ) < 1 implies that the mapping Ax is a contraction mapping in any pno rm on R"?

Exercise 2.15 Consider the nonlinear equations

where I € ) < $. Using the contraction mapping principle, show that the equations have a unique real solution.

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2.6. EXERCISES 91

Exercise 2.16 Let f : Rn -+ R" be locally Lipschitz in a domain D C R". Let S c D be a compact set. Show that there is a positive constant L such that for all Z,Y E S,

Ilf(z) - f(y)II 5 Lllz - yll

Hint : The set S can be covered by a finite number of neighborhoods; that is,

Consider the following two cases separately:

z, y E S n N(a,, ri) for some i.

r z , y 6 S n N(a;, ri) for any i; in this case, llz - yll > mini ri.

In the second case, use the fact that f(z) is uniformly bounded on S.

Exercise 2.17 Show that i f f : Rn - Rn is Lipschitz on W C Rn, then f(z) is uniformly continuous on W.

Exercise 2.18 Show that if f : Rn - R" is Lipschitz on a domain D = {z E Rn I llzll < r} and f(0) = 0, then there is a positive constant k such that llf(z)ll 5 kllzll for all z E D.

Exercise 2.19 For any z E Rn - 10) and any p E [I, oo), define y E Rn by

s-1

Show that yTz = IIz(lp and llylls = 1, where q E (l,oo] is determined from l /p + l / q = 1. For p = cm, find a vector y such that yTz = llzllrn and (Iy(I1 = 1.

Exercise 2.20 Prove Lemma 2.4

Exercise 2.21 Let ( 1 .II, and 11 . [ I p be two different norms of the class of pnorms on Rn. Show that f : R" + R" is Lipschitz in II.I(, if and only if it is Lipschitz in

I I . IIP.

Exercise 2.22 Consider the initial value problem (2.1) and let D C Rn he a do- main that contains z = 0. Suppose f ( t , 0) = 0, f ( t , I) is Lipschitz in z on [to, m ) x D with a Lipschitz constant L in ( 1 . 112, and z(t), the solution of (2.1), is defined for all t 2 to and belongs to D.

(a) Show that

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92 CHAPTER 2. FUNDAMENTAL PROPERTIES

(b) Show that

Exercise 2.23 Let x : R -+ R" be a differentiable function that satisfies

Show that t

I I Z ( ~ ) I I 5 I I Z ( ~ O ) I I + J g(s) ds t o

Exercise 2.24 ([36]) Give another proof of Theorem 2.2 by direct application of the contraction principle in the space of continuous functions with the norm

Exercise 2.25 ([?I) Let f : R -+ R. Suppose f satisfies the inequality

in some neighborhood of zo. Show that f is continuous at za if a > 0, and differ- entiable a t zo if a > 1.

Exercise 2.26 For each of the following functions f : R + R, find whether (a) f is continuously differentiable a t x = 0; (b) f is locally Lipschitz a t z = 0; (c) f is continuous at z = 0; (d) f is globally Lipschitz; (e) f is uniformly continuous on R; (f) f is Lipschitz on (-1, 1).

x2sin( l /z) , for z # 0 (1) f (x) =

for z = 0 { i n ( l / x ) for z # 0 (2) f ( x ) =

for z = 0

(3) f (z) = tan(?iz/Z)

Exercise 2.27 For each of the following functions f : Rn - Rn, find whether (a) f is continuously differentiable; (h) f is locally Lipschitz; (c) f is continuous; (d) f is globally Lipschitz; (e) f is uniformly continuous on R".

21 + sgn (22) z l +sa t (x2) XI + sin z2 I

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2.6. EXERCISES 93

Exercise 2.28 Let D, = {z E Rn 1 11x11 < r). For each of the following systems, represented as t = f ( t , z ) , find whether (a) f is locally Lipschitz in z on D,, for sufficiently small r; (b) f is locally Lipschitz in z on D,, for any finite r > 0; (c) f is globally Lipschitz in z.

(1) The pendulum equation with friction and constant input torque (Section 1.1.1).

(2) The tunnel diode circuit (Example 1.2).

(3) The mass-spring equation with linear spring, linear viscous damping, dry fric- tion, and zero external force (Section 1.1.3).

(4) The Van der Pol oscillator (Example 1.7),

(5) The closed-loop equation of a third-order adaptive control system (Section 1.1.6).

(6) The system i: = Az - B$(Cz), where A, B, and C a r e n x n, n x 1, and 1 x n matrices, respectively, and $(.) is a dead-zone nonlinearity, defined by

y + d , f o r y < - d $(Y) = 0, for - d < y _ < d

y - d, for y > d

Exercise 2.29 Show that if fi : R -+ R and f2 : R - R are locally Lipschitz, then fi + f2, fl f2 and f2 o f l are locally Lipschitz.

Exercise 2.30 Let f : R" - R" he defined by

where g : Rn i R is locally Lipschitz and nonnegative, and K is a constant matrix. Show that f(x) is Lipschitz on any compact subset of R".

Exercise 2.31 Let V : R x Rn + R he continuously differentiable. Suppose V ( t , 0) = 0 for all t 2 0 and

where cl and c4 are positive constants and D C Rn is a convex domain that contains the origin z = 0.

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94 CHAPTER 2. FUNDAMENTAL PROPERTIES

( a ) Show that V ( t , x ) < $~4/ Ix11~ for all x E D. Hint : Use the representation V ( t , x ) = J: g ( t , u x ) d u x.

(b ) Show that the constants cl and c4 must satisfy 2cl < c4 (c) Show that W ( t , x ) = satisfies the Lipschitz condition

Exercise 2.32 Let f ( t , x ) be piecewise continuous in t and locally Lipschitz in x on [to, t l ] x D , for some domain D c Rn. Let W be a compact subset of D. Let z(t' be the solution of x = f ( t , x ) starting at x( to) = z o E W . Suppose x ( t ) is defined and x ( t ) E W for all t E [ t o , T ) , T < t l .

( a ) Show that z ( t ) is uniformly continuous on [ to ,T) .

(b) Show that z ( T ) is defined and belongs to W , and z ( t ) is a solution on [ to ,Tl .

(c) Show that there is 6 > 0 such that the solution can be extended t o [ to ,T + 61.

Exercise 2.33 Let f ( t , x ) be piecewise continuous in t and locally Lipschitz in x on [to, t l ] x D, for some domain D C R". Let y( t ) be a solution of (2.1) on a maximal open interval [ to ,T) C [to,t l] with T < a. Let W be any compact subset of D. Show that there is some t E [ to ,T) with y( t ) @ W . Hint : Use the previous exercise.

Exercise 2.34 Let f ( t , x ) be piecewise continuous in t , locally Lipschitz in x , and

( a ) Show that the solution of (2.1) satisfies

kl Il~(t)l l 5 llxoll exp[kz(t - to)] + -{exp[kz(t kz - t o ) ] - 1)

for all t >_ to for which the solution exists

(b ) Can the solution have a finite escape time?

Exercise 2.35 Let g : Rn -t Rn be continuously differentiable for all x E Rn, and define f ( x ) by

Show that 2: = f ( x ) , x (0 ) = xo, has a unique solution defined for all t > 0.

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Exercise 2.36 Show that the state equation

has a unique solution defined for all t 2 0.

Exercise 2.37 Suppose the second-order system i = f(x), with a locally Lipschitz f (z ) , has a limit cycle. Show that any solution that starts in the region enclosed by the limit cycle cannot have a finite escape time.

Exercise 2.38 ([36]) Let z l : R + Rn and 2 2 : R + Rn he differentiable func- tions such that

I - I 5 7 Ilxi(t) - f((t,zi(t))ll 5 pi , for i = l , 2

for a 5 t 5 b. I f f satisfies the Lipschitz condition (2.2), show that

Exercise 2.39 Derive the sensitivity equations for the tunnel diode circuit of Ex- ample 1.2 as L and C vary from their nominal values.

Exercise 2.40 Derive the sensitivity equations for the Van der Pol oscillator of Example 1.7 as r varies from its nominal value. Use the state equation in the z-coordinates.

Exercise 2.41 Repeat the previous exercise using the state equation in the z- coordinates.

Exercise 2.42 Derive the sensitivity equations for the system 1

X I = tan- (azl) - ~ 1 x 2

x2 = bzf - cx2

as the parameters a , b, c vary from their nominal values ao = 1, ba = 0, and co = 1.

Exercise 2.43 Let f (z ) be continuously differentiable, f(0) = 0, and

- %(o) 5 ~ i ~ ~ z ~ ~ 2 , for 1 5 i 5 n a f i 112

Show that -

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96 CHAPTER 2. FUNDAMENTAL PROPERTIES

Exercise 2.44 Show, under the assumptions of Theorem 2.6, that the solution of (2.1) depends continuously on the initial time to.

Exercise 2.45 Let f (t, x) and its partial derivative with respect to z be continuous in (t, z) for all (t, z) E [to, tl] x Rn. Let z(t,q) he the solution of (2.1) that starts at c(to) = 7 and suppose x(t,q) is defined on [to, tl]. Show that x(t, q) is continuously differentiable with respect to 7 and find the variational equation satisfied by [ax/av]. Hint: Put y = z - q to transform (2.1) into

with q as a parameter.

Exercise 2.46 Let f( t , z) and its partial derivative with respect to z he continuous in (t,x) for all (t ,x) E R x Rn. Let z(t, a , q) he the solution of (2.1) that starts at z(a) = q and suppose that z(t, a, q) is defined on [a, tl]. Show that x(t, a , 7) is continuously differentiable with respect to a and q and let z.(t) and z,(t) denote [axlaa] and [azlaq], respectively. Show that x,(t) and x,(t) satisfy the identity

Exercise 2.47 ([36]) Let f : R x R i R be a continuous function. Suppose f( t , z) is locally Lipschitz and nondecreasing in x for each fixed value o f t . Let x(t) be a solution of x = f ( t , z) on an interval [a, b]. If the continuous function y(t) satisfies the integral inequality

for a < t < b, show that y(t) < x(t) throughout this interval,