CHAPTER 4 DESIGN OF STATE FEEDBACK CONTROLLERS AND STATE OBSERVERS USING REDUCED ORDER MODEL

Size: px
Start display at page:

Download "CHAPTER 4 DESIGN OF STATE FEEDBACK CONTROLLERS AND STATE OBSERVERS USING REDUCED ORDER MODEL"

Transcription

1 98 CHAPTER DESIGN OF STATE FEEDBACK CONTROLLERS AND STATE OBSERVERS USING REDUCED ORDER MODEL INTRODUCTION The deign of ytem uing tate pace model for the deign i called a modern control deign and it i having an advantage of providing a complete (internal) decription of the ytem The power of tate variable method i the deign can be done with more than one control input and alo the inner variable (tate variable) are ued for feedback for atifying the deired performance Darouach et al (99) dealt with a method baed on the generalized contrained Sylveter equation for the deign of reduced order oberver for decriptor ytem with unknown input New condition for the exitence of reduced-order linear functional tate oberver for linear ytem with unknown input were preented by Trinh et al () Sytematic procedure for the ynthei of reduced-order functional oberver were given It i tated that the attractive feature of the propoed oberver wa the implicity with which the deign proce can be accomplihed Illutrative example had been given to illutrate the attractivene and implicity of the deign procedure Weiwen and Zhigiang () preented a comparion tudy of performance and characteritic of three advanced tate oberver, including the high-gain oberver, the liding-mode oberver and the extended tate

2 99 oberver Thee oberver were originally propoed to addre the dependence of the claical oberver, uch a the Kalman filter and the Luenberger oberver, on the accurate mathematical repreentation of the plant It wa oberved that, the extended tate oberver wa much uperior in dealing with dynamic uncertaintie, diturbance and enor noie Several novel nonlinear gain function were propoed to addre the difficulty in dealing with unknown initial condition with imulation and experimental reult In thi chapter, tate controller and oberver are deigned uing the reduced econd order model obtained uing the uggeted technique Example from chapter are conidered for the deign of tate controller and tate oberver State Feedback Controller The main objective in the deign of tate feedback control i to yield deirable cloed loop repone in term of both tranient and teady tate characteritic For the deign of tate feedback controller, pole placement i the technique which i ued to place the cloed loop pole of the ytem in pre determined location The location of pole correpond directly to the Eigen value of the ytem, which can control the characteritic of the ytem If the open loop ytem i tate controllable in nature, then an arbitrary cloed loop eigen value uing the tate feedback can be eaily achieved State Oberver In the control ytem deign, tate feedback require all the tate variable for all the time In mot of the practical ituation, the availability of all the tate variable for the meaurement i not poible and for uch cae,

3 if the ytem i completely obervable with a given et of output, then it i poible to determine the tate Thee tate are not directly meaured and their Eigen value can be arbitrarily aigned uing tate feedback State oberver i a device, which provide an etimate of the unknown internal tate of the ytem from the input and output of the correponding ytem DESIGN OF STATE FEEDBACK CONTROLLER FOR LTICS Conider an n th order table linear time invariant ytem decribed by the tranfer function given in Equation (): G ( ) b m n m b a b m m m m () n n n an a b where, a i ( i n) and b i ( i m) are calar contant and mn The tate model of Equation () in controllable canonical form i given a in Equation () and () x Ax Bu () y Cx Du () where, u i the input y i the output x i the tate vector

4 A i the tate vector a n a a a A B i the input vector B C i the output vector Auming that the pair (A, B) i controllable there exit a feedback matrix K uch that cloed loop ytem Eigen value can be placed in arbitrary location The repreentation of the ytem with tate feedback i repreented in Figure Figure Repreentation of Sytem with tate feedback

5 The control law i given in Equation () u Kx () where, Gain matrix n k k k K The cloed loop dynamic of the ytem i e the ytem with tate feedback controller i repreented in Equation () and (): ) ( BK A I () ) ( ) ( ) ( ) ( ) ( n a n k k a k a k a BK A () Thu the problem i to find K o that the deired characteritic polynomial of (A-BK) matche the deired characteritic polynomial Therefore the tranfer function of ytem given in Equation () with tate feedback controller i a in Equation () ) ( ) ( ) ( ) ( k a k a k a b b b b G n n n n n n n m m m m m m contr ()

6 Peudo Code for the Deign of State Feedback Controller for LTICS Get the higher order original ytem in tate pace model a in Equation () and () If (ytem i controllable) { If(order of the ytem>) { Convert the tate pace model into tranfer function Reduce into econd order ytem uing algorithm explained in chapter Convert the tranfer function into controllable canonical tate model } Calculate the value of the tate feedback controller gain matrix K by comparing the deired and characteritic polynomial Tune the value of K uing PSO Contruct the tranfer function for the reduced ytem with tate feedback controller From tep, derive the tranfer function of original ytem with controller Verify the repone of the ytem with and without controller } Endif

7 Algorithm to Deign State Feedback Controller for LTICS Step : Get the higher order original ytem in tate pace model a in Equation () and () Step : Check for the controllability of the given ytem Step : Convert the tate pace model into tranfer function model uing the Equation (8): G ( ) C ( I A ) B (8) Step : Uing the propoed method of model reduction explained in chapter, convert the higher order tranfer function given in (8) into econd order model Step : Obtain the controllable canonical form (phae variable form) of the econd order reduced model a written in Equation () and () Step : Uing the tate model of reduced ytem, obtain the characteritic polynomial of the given ytem uing the Equation (9) I A (9) +a + a = () where a and a are the coefficient of the polynomial Step : Get the deired pecification ettling time and percentage overhoot Uing the pecification, calculate the deired damping ratio () and natural frequency of ocillation ( n ) Step 8: Uing Equation (), the deired characteritic polynomial i obtained a in Equation ()

8 + n + n = () where i the damping ratio and n i the natural frequency of ocillation S + = () where, and are the coefficient of the polynomial Step 9: The tate feedback gain matrix i calculated uing Equation () and () a: K=[( -a ) ( -a )] () Step : The value of gain matrix K are tuned uing PSO in uch a way that the deired pecification are met Step : Uing the calculated gain matrix K in Equation (), the controllable canonical form of the reduced model with tate feedback controller R contr tranfer function i alo calculated i contructed and the correponding Step : From the tranfer function of reduced model with tate feedback controller obtained in tep, the tranfer function of the original ytem with tate feedback controller revering the procedure of model reduction G contr i contructed by Step : By comparing original higher order ytem hown in Equation () and G contr, controller gain matrix i calculated Step : Verify the tep repone of the G contr, for the deired pecification

9 DESIGN OF STATE FEEDBACK CONTROLLER FOR LTIDS and Equation () The tate model for the dicrete ytem i given in Equation () x( k ) Ax( k) Bu( k) () y( k) Cx( k) Du( k) () where, x i the tate vector A i the tate vector of ize nxn B i the input vector of ize nx C i the output vector of ize xn D i the tate vector of ize nxn For the ytem to be completely controllable, the control law i given in Equation () u( k) Kx () where, Gain matrix K k k k n The cloed loop dynamic of the ytem i e the ytem with tate feedback controller i hown in Equation () and ()

10 Peudo Code for the Deign of State Feedback Controller for LTIDS Get the higher order original ytem in tate pace model a in Equation () and () If (ytem i controllable) { If (order of the ytem>) { Convert the tate pace model into tranfer function Reduce into econd order ytem uing algorithm given in Chapter Convert the tranfer function into controllable canonical tate model } Calculate the value of the tate feedback controller gain matrix K by comparing the deired and characteritic polynomial Tune the value of K uing PSO Contruct the tranfer function for the reduced ytem with tate feedback controller From above tep derive the tranfer function of original ytem with controller Verify the repone of the ytem with and without controller } Endif

11 8 Algorithm to Deign State Feedback Controller for LTIDS Step : Get the higher order original ytem in tate pace model a in Equation () and () Step : Check for the controllability of the given ytem uing Ackerman formula Step : Obtain the tranfer function model of the given dicrete ytem uing () and check for the pecification G ( z ) C ( zi A) B () Step : If the pecification are not met, convert into continuou domain uing tranformation technique and obtain the reduced model in continuou domain Step : Uing the algorithm explained in ection, deign tate feedback controller and obtain the gain matrix K for reduced model The value are tuned uing PSO in uch a way that the required pecification are met Step : Convert the continuou model into dicrete model uing invere tranformation technique Step : Contruct the higher order dicrete time tranfer function uing the invere procedure of model reduction Step 8: Verify the deired pecification

12 9 ILLUSTRATIONS Example Conider a higher order ytem in the context of Palaniwami et al () hown in tate pace a: A ; B C ; D The tranfer function of the given ytem i obtained uing Equation (8) a: ) ( 8 S G

13 The econd order model uing the propoed method of model reduction explained in Chapter ection i: 9 98 R ( ) 99 9 On rearranging the above equation, R ( ) (8) 8 9 The controllable canonical form of the reduced model i derived in Equation (9) uing Equation () and (): A ; 9 8 B ; C ] ; D (9) For a choice of deigner pecification hown in ection, the characteritic polynomial in Equation () i obtained uing Equation () a: +8+9= () with ettling time t ec percentage overhoot% damping ratio =9 and natural frequency of ocillation n = 8 The deired characteritic polynomial in Equation () i obtained uing Equation () ++9= ()

14 Therefore, the gain matrix K i calculated a: K=[988 8] The value of the K matrix are tuned uing PSO and the tuned value of K are obtained a: K= [ 8] The tranfer function of reduced model with tate feedback controller i given in Equation R contr ( ) () 9 By revering the procedure of model reduction, the tranfer function of the original ytem with tate controller i calculated a in Equation (): G contr ( S ) The gain of the original ytem i, () K= [ ] The tep repone of the original ytem and reduced ytem with the deigned tate feedback controller are hown in Figure and

15 8 Step Repone of Original Sytem without and with State Controller Original ytem Original ytem with State Controller Output Time (econd) Figure Comparion of tep repone of original ytem with and without tate controller of Example 8 Step Repone of Reduced Sytem without and with State Controller Reduced ytem Reduced ytem with State Controller Output Time (econd) Figure Comparion of tep repone of reduced ytem with and without tate controller of Example

16 From Figure and, it i oberved that propoed reduced ytem with tate feedback controller follow the original ytem with tate feedback controller Both the repone indicate that the overhoot preent in the original ytem i completely eliminated Here the deign complexity i reduced by uing the econd order model Example Conider the given third order ytem: A ; B C D The tranfer function model for the given ytem in Equation i obtained uing Equation (8) G ( ) () By uing the propoed method of model reduction, the reduced model of Equation () i obtained a in Equation () R ( ) () 8 8

17 On rearranging the above equation, 8 R ( ) () Equation () The characteritic polynomial from Equation () i written a in ++= () By comparing Equation () with deired characteritic polynomial repreented in Equation (), the gain matrix i calculated a: K= [ 9] The value are tuned uing PSO and the tuned value are: K= [ ] With the tate feedback controller, the tranfer function of the reduced ytem i obtained a in Equation (8): 8 R contr ( ) (8) 8 The tranfer function of original ytem with controller i obtained by revering the procedure of model reduction The tranfer function i obtained a in Equation (9) G contr ( ) (9) 9 9 The tep repone of original and reduced ytem with and without tate feedback controller are given in Figure () and ()

18 Step Repone of Original Sytem without and with State Controller Original ytem Original ytem with State Controller Output 8 8 Time (econd) Figure Comparion of tep repone of original ytem with and without tate controller of Example Step Repone of Reduced Sytem without and with State Controller Reduced ytem Reduced ytem with State Controller Output 8 8 Time (econd) Figure Comparion of tep repone of reduced ytem with and without tate controller of Example

19 From the tep repone of propoed reduced ytem with tate feedback controller and original ytem with tate feedback controller hown in Figure and, it i oberved that it i poible to deign a tate feedback controller only with the reduced econd order model to atify the deigner pecification Both the repone indicate that the maximum peak overhoot preent in the original ytem i minimied Example Conider eighth order dicrete ytem from Ravichandran et al (), A ; B C ;

20 The tranfer function of the given ytem i obtained a: ( 8z z z z z z z 8 G z) 8 8z z 8z z z 8z 8z z 8 () The eighth order original ytem i tranformed into G () a in Equation () by uing Bilinear tranformation, z 8 9 G S) ( () Uing the propoed algorithm of model reduction, the reduced model i obtained a in Equation (): 99 R ( ) () 8 On rearranging the above Equation () 8 R ( ) () 9 8 Equation () The controllable form tate model of Equation () i given in A ; B 8 9 ; C 8 ; D ()

21 8 Equation The characteritic polynomial of Equation () i given in +9+8= () For the choice of performance pecification given in ection, the deired characteritic polynomial i obtained a in Equation () ++9= () Therefore the gain matrix K i calculated uing Equation () and () a: K=[ 988] Uing PSO, the value of the K matrix are tuned and the tuned value of controller gain matrix K are K= [ ] Therefore, the tranfer function of reduced ytem with tate feedback controller i given in Equation 8 R contr ( ) () 8 By applying the invere tranformation technique, the reduced domain model of Equation () i converted into dicrete model a in Equation (8) z 8 R contr ( z) (8) z 8z The controller gain matrix in dicrete domain i: K= [-9 ]

22 9 The tranfer function of given higher order dicrete ytem Equation (9) i obtained by applying invere reduction procedure to Equation (8) G contr 8z z z z z z z 8 ( z) 8 8z z 8z z z 8z 8z z 8 (9) The comparion of tep repone of original and reduced ytem with tate controller i hown in Figure () and () It i depicted that the ytem with tate feedback controller produce minimum rie time, ettling time and peak overhoot Comparion of Step Repone of Original Sytem with and without tate controller 8 Original ytem Original ytem with tate controller Output Sampling intant Figure Comparion of tep repone of reduced ytem with and without tate controller of Example

23 Comparion of Step Repone of Reduced Sytem with and without tate controller 8 Reduced ytem Reduced ytem with tate controller Output Sampling intant Figure Comparion of tep repone of reduced ytem with and without tate controller of Example DESIGN OF STATE OBSERVER In the deign of tate oberver, the oberver gain G i elected in uch a way that the continuou error dynamic converge to zero aymptotically Conider linear time invariant ytem hown in Equation () and Equation () The error dynamic i given by (A - GC) If thi i table in nature, the error vector will converge to zero for any initial error i e the etimated value reache the original value, where G i the oberver gain matrix

24 Peudo Code for State Oberver Deign Get the higher order original ytem in tate pace model a in Equation () and Equation () If ( ytem i LTIDS) {If (ytem i Obervable) {If(order of the ytem>) { Convert the tate pace model into tranfer function Reduce into econd order ytem uing the propoed algorithm explained in chapter ection Convert the tranfer function into obervable form of tate model } Calculate the value of the tate oberver gain matrix by comparing the deired and characteritic polynomial Tune the value of Oberver gain matrix uing PSO and obtain optimized value Contruct the tranfer function for the reduced ytem with tate oberver Derive the tranfer function of original ytem with oberver Convert LTICS into LTIDS Verify the repone of the ytem with and without oberver Endif } Endif

25 Algorithm for State oberver Deign Step : Step : Step : Step : Step : Step : Step : Get the higher order ytem Check for the obervability of the ytem If the ytem i obervable, convert the tate model into tranfer function model by uing Equation (8) Check for the deired pecification If the pecification are not met, derive the reduced model for the given ytem uing the propoed method of model reduction a in Equation () and obtain the obervable phae variable form of it Obtain the characteritic polynomial of reduced ytem a in Equation () From the deired characteritic, derive the deired polynomial a in Equation () From Equation () and () determine the oberver gain matrix a: a G a Step 8: Step 9: The value of G are tuned uing PSO to get the deired pecification Uing the tune value of G, obtain the tate pace model of reduced ytem with oberver Step : The tranfer function of reduced ytem with tate oberver i obtained from tate pace model Step : The tranfer function of the original ytem with tate oberver i obtained from reduced ytem with tate oberver by applying invere procedure of model reduction

26 ILLUSTRATIONS Example (): Conider the eighth order ytem function from Palaniwami et al ( G S) Uing the propoed method explained in Chapter ection, the econd order model i obtained a: R 9 98 ) 99 9 ( On rearranging the above equation, R ( ) () 8 9 By conidering the deired characteritic polynomial given in Equation () and characteritic polynomial from Equation (), the oberver gain matrix i obtained a: G The value are tuned uing Particle Swarm Optimiation The parameter for the tuning proce are elected from ection to get the deired performance The Gain matrix with tuned value i, G

27 Therefore the tranfer function of reduced ytem with tate oberver i obtained in Equation () R ob ( ) () 8 By applying the revere procedure of model reduction, the tranfer function of original ytem with tate oberver i obtained in Equation () G ob (S) () The comparion of tep repone i given in Figure 8 and 9 The tate oberver deigned uing the propoed econd order ytem atifie atifying the deired pecification of repone without overhoot Hence the deign complexity i reduced in the proce deigning tate oberver for a higher order ytem 8 Step Repone of Original Sytem without and With tate oberver Original ytem Original ytem with tate oberver Output 8 Figure Time Comparion of tep repone of original ytem with and without tate oberver of Example

28 8 Step Repone of Reduced Sytem without and With tate oberver Reduced ytem Reduced ytem with tate oberver Output 8 Figure Time Comparion of tep repone of reduced ytem with and without tate oberver of Example Deign of State controller from State oberver: The characteritic polynomial i obtained from Equation () a: 8 The value of Gain matrix i obtained a: K=[9 -] The value are tuned uing PSO and the tuned value are: K=[ -88] Uing the tuned gain matrix the tranfer function of the reduced order ytem with tate controller i given in Equation () R con ( ) () 9 8 By applying the revere procedure of model reduction, the tranfer function of original ytem with tate controller i obtained a in Equation ()

29 G( S) () The Figure () how the comparion of tep repone of original ytem with and without tate controller 8 Step Repone of original Sytem without and With tate Controller Original ytem original ytem with tate controller Output Time (econd) Figure Comparion of tep repone of original ytem with and without tate controller of Example SUMMARY The deign of tate feedback controller and oberver uing propoed econd order model i explained through illutrative example elected from Chapter From the tep repone of the propoed reduced ytem with tate feedback controller and original ytem with tate feedback controller for variou Example, it i oberved that the deign complexity can be reduced by uing imple econd order model The tate oberver deigned uing the propoed econd order ytem alo atifie the deired pecification of repone without overhoot Hence the deign complexity i reduced in the proce deigning tate oberver for a higher order ytem

CHAPTER 8 OBSERVER BASED REDUCED ORDER CONTROLLER DESIGN FOR LARGE SCALE LINEAR DISCRETE-TIME CONTROL SYSTEMS

CHAPTER 8 OBSERVER BASED REDUCED ORDER CONTROLLER DESIGN FOR LARGE SCALE LINEAR DISCRETE-TIME CONTROL SYSTEMS CHAPTER 8 OBSERVER BASED REDUCED ORDER CONTROLLER DESIGN FOR LARGE SCALE LINEAR DISCRETE-TIME CONTROL SYSTEMS 8.1 INTRODUCTION 8.2 REDUCED ORDER MODEL DESIGN FOR LINEAR DISCRETE-TIME CONTROL SYSTEMS 8.3

More information

Module 4: Time Response of discrete time systems Lecture Note 1

Module 4: Time Response of discrete time systems Lecture Note 1 Digital Control Module 4 Lecture Module 4: ime Repone of dicrete time ytem Lecture Note ime Repone of dicrete time ytem Abolute tability i a baic requirement of all control ytem. Apart from that, good

More information

Evolutionary Algorithms Based Fixed Order Robust Controller Design and Robustness Performance Analysis

Evolutionary Algorithms Based Fixed Order Robust Controller Design and Robustness Performance Analysis Proceeding of 01 4th International Conference on Machine Learning and Computing IPCSIT vol. 5 (01) (01) IACSIT Pre, Singapore Evolutionary Algorithm Baed Fixed Order Robut Controller Deign and Robutne

More information

State Space: Observer Design Lecture 11

State Space: Observer Design Lecture 11 State Space: Oberver Deign Lecture Advanced Control Sytem Dr Eyad Radwan Dr Eyad Radwan/ACS/ State Space-L Controller deign relie upon acce to the tate variable for feedback through adjutable gain. Thi

More information

Gain and Phase Margins Based Delay Dependent Stability Analysis of Two- Area LFC System with Communication Delays

Gain and Phase Margins Based Delay Dependent Stability Analysis of Two- Area LFC System with Communication Delays Gain and Phae Margin Baed Delay Dependent Stability Analyi of Two- Area LFC Sytem with Communication Delay Şahin Sönmez and Saffet Ayaun Department of Electrical Engineering, Niğde Ömer Halidemir Univerity,

More information

A Simplified Methodology for the Synthesis of Adaptive Flight Control Systems

A Simplified Methodology for the Synthesis of Adaptive Flight Control Systems A Simplified Methodology for the Synthei of Adaptive Flight Control Sytem J.ROUSHANIAN, F.NADJAFI Department of Mechanical Engineering KNT Univerity of Technology 3Mirdamad St. Tehran IRAN Abtract- A implified

More information

Massachusetts Institute of Technology Dynamics and Control II

Massachusetts Institute of Technology Dynamics and Control II I E Maachuett Intitute of Technology Department of Mechanical Engineering 2.004 Dynamic and Control II Laboratory Seion 5: Elimination of Steady-State Error Uing Integral Control Action 1 Laboratory Objective:

More information

THE PARAMETERIZATION OF ALL TWO-DEGREES-OF-FREEDOM SEMISTRONGLY STABILIZING CONTROLLERS. Tatsuya Hoshikawa, Kou Yamada and Yuko Tatsumi

THE PARAMETERIZATION OF ALL TWO-DEGREES-OF-FREEDOM SEMISTRONGLY STABILIZING CONTROLLERS. Tatsuya Hoshikawa, Kou Yamada and Yuko Tatsumi International Journal of Innovative Computing, Information Control ICIC International c 206 ISSN 349-498 Volume 2, Number 2, April 206 pp. 357 370 THE PARAMETERIZATION OF ALL TWO-DEGREES-OF-FREEDOM SEMISTRONGLY

More information

MODERN CONTROL SYSTEMS

MODERN CONTROL SYSTEMS MODERN CONTROL SYSTEMS Lecture 1 Root Locu Emam Fathy Department of Electrical and Control Engineering email: emfmz@aat.edu http://www.aat.edu/cv.php?dip_unit=346&er=68525 1 Introduction What i root locu?

More information

CONTROL OF INTEGRATING PROCESS WITH DEAD TIME USING AUTO-TUNING APPROACH

CONTROL OF INTEGRATING PROCESS WITH DEAD TIME USING AUTO-TUNING APPROACH Brazilian Journal of Chemical Engineering ISSN 004-6632 Printed in Brazil www.abeq.org.br/bjche Vol. 26, No. 0, pp. 89-98, January - March, 2009 CONROL OF INEGRAING PROCESS WIH DEAD IME USING AUO-UNING

More information

Digital Control System

Digital Control System Digital Control Sytem - A D D A Micro ADC DAC Proceor Correction Element Proce Clock Meaurement A: Analog D: Digital Continuou Controller and Digital Control Rt - c Plant yt Continuou Controller Digital

More information

NONLINEAR CONTROLLER DESIGN FOR A SHELL AND TUBE HEAT EXCHANGER AN EXPERIMENTATION APPROACH

NONLINEAR CONTROLLER DESIGN FOR A SHELL AND TUBE HEAT EXCHANGER AN EXPERIMENTATION APPROACH International Journal of Electrical, Electronic and Data Communication, ISSN: 232-284 Volume-3, Iue-8, Aug.-25 NONLINEAR CONTROLLER DESIGN FOR A SHELL AND TUBE HEAT EXCHANGER AN EXPERIMENTATION APPROACH

More information

Chapter 7. Root Locus Analysis

Chapter 7. Root Locus Analysis Chapter 7 Root Locu Analyi jw + KGH ( ) GH ( ) - K 0 z O 4 p 2 p 3 p Root Locu Analyi The root of the cloed-loop characteritic equation define the ytem characteritic repone. Their location in the complex

More information

EE 4443/5329. LAB 3: Control of Industrial Systems. Simulation and Hardware Control (PID Design) The Inverted Pendulum. (ECP Systems-Model: 505)

EE 4443/5329. LAB 3: Control of Industrial Systems. Simulation and Hardware Control (PID Design) The Inverted Pendulum. (ECP Systems-Model: 505) EE 4443/5329 LAB 3: Control of Indutrial Sytem Simulation and Hardware Control (PID Deign) The Inverted Pendulum (ECP Sytem-Model: 505) Compiled by: Nitin Swamy Email: nwamy@lakehore.uta.edu Email: okuljaca@lakehore.uta.edu

More information

Lecture 4. Chapter 11 Nise. Controller Design via Frequency Response. G. Hovland 2004

Lecture 4. Chapter 11 Nise. Controller Design via Frequency Response. G. Hovland 2004 METR4200 Advanced Control Lecture 4 Chapter Nie Controller Deign via Frequency Repone G. Hovland 2004 Deign Goal Tranient repone via imple gain adjutment Cacade compenator to improve teady-tate error Cacade

More information

ME 375 FINAL EXAM Wednesday, May 6, 2009

ME 375 FINAL EXAM Wednesday, May 6, 2009 ME 375 FINAL EXAM Wedneday, May 6, 9 Diviion Meckl :3 / Adam :3 (circle one) Name_ Intruction () Thi i a cloed book examination, but you are allowed three ingle-ided 8.5 crib heet. A calculator i NOT allowed.

More information

Digital Control System

Digital Control System Digital Control Sytem Summary # he -tranform play an important role in digital control and dicrete ignal proceing. he -tranform i defined a F () f(k) k () A. Example Conider the following equence: f(k)

More information

CALIFORNIA INSTITUTE OF TECHNOLOGY Control and Dynamical Systems

CALIFORNIA INSTITUTE OF TECHNOLOGY Control and Dynamical Systems Control and Dynamical Sytem CDS 0 Problem Set #5 Iued: 3 Nov 08 Due: 0 Nov 08 Note: In the upper left hand corner of the econd page of your homework et, pleae put the number of hour that you pent on thi

More information

Sliding Mode Control of a Dual-Fuel System Internal Combustion Engine

Sliding Mode Control of a Dual-Fuel System Internal Combustion Engine Proceeding of the ASME 9 Dynamic Sytem and Control Conference DSCC9 October -4, 9, Hollywood, California, USA DSCC9-59 Control of a Dual-Fuel Sytem Internal Combution Engine Stephen Pace Department of

More information

NAME (pinyin/italian)... MATRICULATION NUMBER... SIGNATURE

NAME (pinyin/italian)... MATRICULATION NUMBER... SIGNATURE POLITONG SHANGHAI BASIC AUTOMATIC CONTROL June Academic Year / Exam grade NAME (pinyin/italian)... MATRICULATION NUMBER... SIGNATURE Ue only thee page (including the bac) for anwer. Do not ue additional

More information

Linear System Fundamentals

Linear System Fundamentals Linear Sytem Fundamental MEM 355 Performance Enhancement of Dynamical Sytem Harry G. Kwatny Department of Mechanical Engineering & Mechanic Drexel Univerity Content Sytem Repreentation Stability Concept

More information

into a discrete time function. Recall that the table of Laplace/z-transforms is constructed by (i) selecting to get

into a discrete time function. Recall that the table of Laplace/z-transforms is constructed by (i) selecting to get Lecture 25 Introduction to Some Matlab c2d Code in Relation to Sampled Sytem here are many way to convert a continuou time function, { h( t) ; t [0, )} into a dicrete time function { h ( k) ; k {0,,, }}

More information

ECE-320 Linear Control Systems. Spring 2014, Exam 1. No calculators or computers allowed, you may leave your answers as fractions.

ECE-320 Linear Control Systems. Spring 2014, Exam 1. No calculators or computers allowed, you may leave your answers as fractions. ECE-0 Linear Control Sytem Spring 04, Exam No calculator or computer allowed, you may leave your anwer a fraction. All problem are worth point unle noted otherwie. Total /00 Problem - refer to the unit

More information

Control of Delayed Integrating Processes Using Two Feedback Controllers R MS Approach

Control of Delayed Integrating Processes Using Two Feedback Controllers R MS Approach Proceeding of the 7th WSEAS International Conference on SYSTEM SCIENCE and SIMULATION in ENGINEERING (ICOSSSE '8) Control of Delayed Integrating Procee Uing Two Feedback Controller R MS Approach LIBOR

More information

MM1: Basic Concept (I): System and its Variables

MM1: Basic Concept (I): System and its Variables MM1: Baic Concept (I): Sytem and it Variable A ytem i a collection of component which are coordinated together to perform a function Sytem interact with their environment. The interaction i defined in

More information

Control Systems Engineering ( Chapter 7. Steady-State Errors ) Prof. Kwang-Chun Ho Tel: Fax:

Control Systems Engineering ( Chapter 7. Steady-State Errors ) Prof. Kwang-Chun Ho Tel: Fax: Control Sytem Engineering ( Chapter 7. Steady-State Error Prof. Kwang-Chun Ho kwangho@hanung.ac.kr Tel: 0-760-453 Fax:0-760-4435 Introduction In thi leon, you will learn the following : How to find the

More information

EE Control Systems LECTURE 6

EE Control Systems LECTURE 6 Copyright FL Lewi 999 All right reerved EE - Control Sytem LECTURE 6 Updated: Sunday, February, 999 BLOCK DIAGRAM AND MASON'S FORMULA A linear time-invariant (LTI) ytem can be repreented in many way, including:

More information

Simple Observer Based Synchronization of Lorenz System with Parametric Uncertainty

Simple Observer Based Synchronization of Lorenz System with Parametric Uncertainty IOSR Journal of Electrical and Electronic Engineering (IOSR-JEEE) ISSN: 78-676Volume, Iue 6 (Nov. - Dec. 0), PP 4-0 Simple Oberver Baed Synchronization of Lorenz Sytem with Parametric Uncertainty Manih

More information

S_LOOP: SINGLE-LOOP FEEDBACK CONTROL SYSTEM ANALYSIS

S_LOOP: SINGLE-LOOP FEEDBACK CONTROL SYSTEM ANALYSIS S_LOOP: SINGLE-LOOP FEEDBACK CONTROL SYSTEM ANALYSIS by Michelle Gretzinger, Daniel Zyngier and Thoma Marlin INTRODUCTION One of the challenge to the engineer learning proce control i relating theoretical

More information

Root Locus Contents. Root locus, sketching algorithm. Root locus, examples. Root locus, proofs. Root locus, control examples

Root Locus Contents. Root locus, sketching algorithm. Root locus, examples. Root locus, proofs. Root locus, control examples Root Locu Content Root locu, ketching algorithm Root locu, example Root locu, proof Root locu, control example Root locu, influence of zero and pole Root locu, lead lag controller deign 9 Spring ME45 -

More information

DYNAMIC MODELS FOR CONTROLLER DESIGN

DYNAMIC MODELS FOR CONTROLLER DESIGN DYNAMIC MODELS FOR CONTROLLER DESIGN M.T. Tham (996,999) Dept. of Chemical and Proce Engineering Newcatle upon Tyne, NE 7RU, UK.. INTRODUCTION The problem of deigning a good control ytem i baically that

More information

ECE 3510 Root Locus Design Examples. PI To eliminate steady-state error (for constant inputs) & perfect rejection of constant disturbances

ECE 3510 Root Locus Design Examples. PI To eliminate steady-state error (for constant inputs) & perfect rejection of constant disturbances ECE 350 Root Locu Deign Example Recall the imple crude ervo from lab G( ) 0 6.64 53.78 σ = = 3 23.473 PI To eliminate teady-tate error (for contant input) & perfect reection of contant diturbance Note:

More information

6.447 rad/sec and ln (% OS /100) tan Thus pc. the testing point is s 3.33 j5.519

6.447 rad/sec and ln (% OS /100) tan Thus pc. the testing point is s 3.33 j5.519 9. a. 3.33, n T ln(% OS /100) 2 2 ln (% OS /100) 0.517. Thu n 6.7 rad/ec and the teting point i 3.33 j5.519. b. Summation of angle including the compenating zero i -106.691, The compenator pole mut contribute

More information

LOW ORDER MIMO CONTROLLER DESIGN FOR AN ENGINE DISTURBANCE REJECTION PROBLEM. P.Dickinson, A.T.Shenton

LOW ORDER MIMO CONTROLLER DESIGN FOR AN ENGINE DISTURBANCE REJECTION PROBLEM. P.Dickinson, A.T.Shenton LOW ORDER MIMO CONTROLLER DESIGN FOR AN ENGINE DISTURBANCE REJECTION PROBLEM P.Dickinon, A.T.Shenton Department of Engineering, The Univerity of Liverpool, Liverpool L69 3GH, UK Abtract: Thi paper compare

More information

CONTROL SYSTEMS, ROBOTICS AND AUTOMATION Vol. VIII Decoupling Control - M. Fikar

CONTROL SYSTEMS, ROBOTICS AND AUTOMATION Vol. VIII Decoupling Control - M. Fikar DECOUPLING CONTROL M. Fikar Department of Proce Control, Faculty of Chemical and Food Technology, Slovak Univerity of Technology in Bratilava, Radlinkého 9, SK-812 37 Bratilava, Slovakia Keyword: Decoupling:

More information

Solutions. Digital Control Systems ( ) 120 minutes examination time + 15 minutes reading time at the beginning of the exam

Solutions. Digital Control Systems ( ) 120 minutes examination time + 15 minutes reading time at the beginning of the exam BSc - Sample Examination Digital Control Sytem (5-588-) Prof. L. Guzzella Solution Exam Duration: Number of Quetion: Rating: Permitted aid: minute examination time + 5 minute reading time at the beginning

More information

Root Locus Diagram. Root loci: The portion of root locus when k assume positive values: that is 0

Root Locus Diagram. Root loci: The portion of root locus when k assume positive values: that is 0 Objective Root Locu Diagram Upon completion of thi chapter you will be able to: Plot the Root Locu for a given Tranfer Function by varying gain of the ytem, Analye the tability of the ytem from the root

More information

Control Systems Analysis and Design by the Root-Locus Method

Control Systems Analysis and Design by the Root-Locus Method 6 Control Sytem Analyi and Deign by the Root-Locu Method 6 1 INTRODUCTION The baic characteritic of the tranient repone of a cloed-loop ytem i cloely related to the location of the cloed-loop pole. If

More information

FRTN10 Exercise 3. Specifications and Disturbance Models

FRTN10 Exercise 3. Specifications and Disturbance Models FRTN0 Exercie 3. Specification and Diturbance Model 3. A feedback ytem i hown in Figure 3., in which a firt-order proce if controlled by an I controller. d v r u 2 z C() P() y n Figure 3. Sytem in Problem

More information

Chapter 13. Root Locus Introduction

Chapter 13. Root Locus Introduction Chapter 13 Root Locu 13.1 Introduction In the previou chapter we had a glimpe of controller deign iue through ome imple example. Obviouly when we have higher order ytem, uch imple deign technique will

More information

Mathematical modeling of control systems. Laith Batarseh. Mathematical modeling of control systems

Mathematical modeling of control systems. Laith Batarseh. Mathematical modeling of control systems Chapter two Laith Batareh Mathematical modeling The dynamic of many ytem, whether they are mechanical, electrical, thermal, economic, biological, and o on, may be decribed in term of differential equation

More information

Stability. ME 344/144L Prof. R.G. Longoria Dynamic Systems and Controls/Lab. Department of Mechanical Engineering The University of Texas at Austin

Stability. ME 344/144L Prof. R.G. Longoria Dynamic Systems and Controls/Lab. Department of Mechanical Engineering The University of Texas at Austin Stability The tability of a ytem refer to it ability or tendency to eek a condition of tatic equilibrium after it ha been diturbed. If given a mall perturbation from the equilibrium, it i table if it return.

More information

Lecture 10 Filtering: Applied Concepts

Lecture 10 Filtering: Applied Concepts Lecture Filtering: Applied Concept In the previou two lecture, you have learned about finite-impule-repone (FIR) and infinite-impule-repone (IIR) filter. In thee lecture, we introduced the concept of filtering

More information

Lecture 8. PID control. Industrial process control ( today) PID control. Insights about PID actions

Lecture 8. PID control. Industrial process control ( today) PID control. Insights about PID actions Lecture 8. PID control. The role of P, I, and D action 2. PID tuning Indutrial proce control (92... today) Feedback control i ued to improve the proce performance: tatic performance: for contant reference,

More information

Finding the location of switched capacitor banks in distribution systems based on wavelet transform

Finding the location of switched capacitor banks in distribution systems based on wavelet transform UPEC00 3t Aug - 3rd Sept 00 Finding the location of witched capacitor bank in ditribution ytem baed on wavelet tranform Bahram nohad Shahid Chamran Univerity in Ahvaz bahramnohad@yahoo.com Mehrdad keramatzadeh

More information

Design By Emulation (Indirect Method)

Design By Emulation (Indirect Method) Deign By Emulation (Indirect Method he baic trategy here i, that Given a continuou tranfer function, it i required to find the bet dicrete equivalent uch that the ignal produced by paing an input ignal

More information

EXTENDED STABILITY MARGINS ON CONTROLLER DESIGN FOR NONLINEAR INPUT DELAY SYSTEMS. Otto J. Roesch, Hubert Roth, Asif Iqbal

EXTENDED STABILITY MARGINS ON CONTROLLER DESIGN FOR NONLINEAR INPUT DELAY SYSTEMS. Otto J. Roesch, Hubert Roth, Asif Iqbal EXTENDED STABILITY MARGINS ON CONTROLLER DESIGN FOR NONLINEAR INPUT DELAY SYSTEMS Otto J. Roech, Hubert Roth, Aif Iqbal Intitute of Automatic Control Engineering Univerity Siegen, Germany {otto.roech,

More information

Then C pid (s) S h -stabilizes G(s) if and only if Ĉpid(ŝ) S 0 - stabilizes Ĝ(ŝ). For any ρ R +, an RCF of Ĉ pid (ŝ) is given by

Then C pid (s) S h -stabilizes G(s) if and only if Ĉpid(ŝ) S 0 - stabilizes Ĝ(ŝ). For any ρ R +, an RCF of Ĉ pid (ŝ) is given by 9 American Control Conference Hyatt Regency Riverfront, St. Loui, MO, USA June -, 9 WeC5.5 PID Controller Synthei with Shifted Axi Pole Aignment for a Cla of MIMO Sytem A. N. Gündeş and T. S. Chang Abtract

More information

Assessment of Performance for Single Loop Control Systems

Assessment of Performance for Single Loop Control Systems Aement of Performance for Single Loop Control Sytem Hiao-Ping Huang and Jyh-Cheng Jeng Department of Chemical Engineering National Taiwan Univerity Taipei 1617, Taiwan Abtract Aement of performance in

More information

A Simple Approach to Synthesizing Naïve Quantized Control for Reference Tracking

A Simple Approach to Synthesizing Naïve Quantized Control for Reference Tracking A Simple Approach to Syntheizing Naïve Quantized Control for Reference Tracking SHIANG-HUA YU Department of Electrical Engineering National Sun Yat-Sen Univerity 70 Lien-Hai Road, Kaohiung 804 TAIAN Abtract:

More information

Chapter #4 EEE8013. Linear Controller Design and State Space Analysis. Design of control system in state space using Matlab

Chapter #4 EEE8013. Linear Controller Design and State Space Analysis. Design of control system in state space using Matlab EEE83 hapter #4 EEE83 Linear ontroller Deign and State Space nalyi Deign of control ytem in tate pace uing Matlab. ontrollabilty and Obervability.... State Feedback ontrol... 5 3. Linear Quadratic Regulator

More information

Function and Impulse Response

Function and Impulse Response Tranfer Function and Impule Repone Solution of Selected Unolved Example. Tranfer Function Q.8 Solution : The -domain network i hown in the Fig... Applying VL to the two loop, R R R I () I () L I () L V()

More information

PIM Digital Redesign and Experiments of a Roll-Angle Controller for a VTOL-UAV

PIM Digital Redesign and Experiments of a Roll-Angle Controller for a VTOL-UAV 1 roceeding of the International Conference on Information and Automation, December 15-1, 5, Colombo, Sri Lanka. IM Digital Redeign and Experiment of a Roll-Angle Controller for a VTOL-UAV Takahi Kahimura*

More information

EE Control Systems LECTURE 14

EE Control Systems LECTURE 14 Updated: Tueday, March 3, 999 EE 434 - Control Sytem LECTURE 4 Copyright FL Lewi 999 All right reerved ROOT LOCUS DESIGN TECHNIQUE Suppoe the cloed-loop tranfer function depend on a deign parameter k We

More information

Robust Decentralized Design of H -based Frequency Stabilizer of SMES

Robust Decentralized Design of H -based Frequency Stabilizer of SMES International Energy Journal: Vol. 6, No., Part, June 005-59 Robut Decentralized Deign of H -baed Frequency Stabilizer of SMES www.erd.ait.ac.th/reric C. Vorakulpipat *, M. Leelajindakrirerk *, and I.

More information

Quantifying And Specifying The Dynamic Response Of Flowmeters

Quantifying And Specifying The Dynamic Response Of Flowmeters White Paper Quantifying And Specifying The Dynamic Repone Of Flowmeter DP Flow ABSTRACT The dynamic repone characteritic of flowmeter are often incompletely or incorrectly pecified. Thi i often the reult

More information

A Comparative Study on Control Techniques of Non-square Matrix Distillation Column

A Comparative Study on Control Techniques of Non-square Matrix Distillation Column IJCTA, 8(3), 215, pp 1129-1136 International Science Pre A Comparative Study on Control Technique of Non-quare Matrix Ditillation Column 1 S Bhat Vinayambika, 2 S Shanmuga Priya, and 3 I Thirunavukkarau*

More information

LOAD FREQUENCY CONTROL OF MULTI AREA INTERCONNECTED SYSTEM WITH TCPS AND DIVERSE SOURCES OF POWER GENERATION

LOAD FREQUENCY CONTROL OF MULTI AREA INTERCONNECTED SYSTEM WITH TCPS AND DIVERSE SOURCES OF POWER GENERATION G.J. E.D.T.,Vol.(6:93 (NovemberDecember, 03 ISSN: 39 793 LOAD FREQUENCY CONTROL OF MULTI AREA INTERCONNECTED SYSTEM WITH TCPS AND DIVERSE SOURCES OF POWER GENERATION C.Srinivaa Rao Dept. of EEE, G.Pullaiah

More information

Multivariable Control Systems

Multivariable Control Systems Lecture Multivariable Control Sytem Ali Karimpour Aociate Profeor Ferdowi Univerity of Mahhad Lecture Reference are appeared in the lat lide. Dr. Ali Karimpour May 6 Uncertainty in Multivariable Sytem

More information

Copyright 1967, by the author(s). All rights reserved.

Copyright 1967, by the author(s). All rights reserved. Copyright 1967, by the author(). All right reerved. Permiion to make digital or hard copie of all or part of thi work for peronal or claroom ue i granted without fee provided that copie are not made or

More information

USING NONLINEAR CONTROL ALGORITHMS TO IMPROVE THE QUALITY OF SHAKING TABLE TESTS

USING NONLINEAR CONTROL ALGORITHMS TO IMPROVE THE QUALITY OF SHAKING TABLE TESTS October 12-17, 28, Beijing, China USING NONLINEAR CONTR ALGORITHMS TO IMPROVE THE QUALITY OF SHAKING TABLE TESTS T.Y. Yang 1 and A. Schellenberg 2 1 Pot Doctoral Scholar, Dept. of Civil and Env. Eng.,

More information

Fractional-Order PI Speed Control of a Two-Mass Drive System with Elastic Coupling

Fractional-Order PI Speed Control of a Two-Mass Drive System with Elastic Coupling Fractional-Order PI Speed Control of a Two-Ma Drive Sytem with Elatic Coupling Mohammad Amin Rahimian, Mohammad Saleh Tavazoei, and Farzad Tahami Electrical Engineering Department, Sharif Univerity of

More information

Wolfgang Hofle. CERN CAS Darmstadt, October W. Hofle feedback systems

Wolfgang Hofle. CERN CAS Darmstadt, October W. Hofle feedback systems Wolfgang Hofle Wolfgang.Hofle@cern.ch CERN CAS Darmtadt, October 9 Feedback i a mechanim that influence a ytem by looping back an output to the input a concept which i found in abundance in nature and

More information

Lqr Based Load Frequency Control By Introducing Demand Response

Lqr Based Load Frequency Control By Introducing Demand Response Lqr Baed Load Frequency Control By Introducing Demand Repone P.Venkateh Department of Electrical and Electronic Engineering, V.R iddhartha Engineering College, Vijayawada, AP, 520007, India K.rikanth Department

More information

Lecture Notes II. As the reactor is well-mixed, the outlet stream concentration and temperature are identical with those in the tank.

Lecture Notes II. As the reactor is well-mixed, the outlet stream concentration and temperature are identical with those in the tank. Lecture Note II Example 6 Continuou Stirred-Tank Reactor (CSTR) Chemical reactor together with ma tranfer procee contitute an important part of chemical technologie. From a control point of view, reactor

More information

Representation of a Group of Three-phase Induction Motors Using Per Unit Aggregation Model A.Kunakorn and T.Banyatnopparat

Representation of a Group of Three-phase Induction Motors Using Per Unit Aggregation Model A.Kunakorn and T.Banyatnopparat epreentation of a Group of Three-phae Induction Motor Uing Per Unit Aggregation Model A.Kunakorn and T.Banyatnopparat Abtract--Thi paper preent a per unit gregation model for repreenting a group of three-phae

More information

An estimation approach for autotuning of event-based PI control systems

An estimation approach for autotuning of event-based PI control systems Acta de la XXXIX Jornada de Automática, Badajoz, 5-7 de Septiembre de 08 An etimation approach for autotuning of event-baed PI control ytem Joé Sánchez Moreno, María Guinaldo Loada, Sebatián Dormido Departamento

More information

Advanced D-Partitioning Analysis and its Comparison with the Kharitonov s Theorem Assessment

Advanced D-Partitioning Analysis and its Comparison with the Kharitonov s Theorem Assessment Journal of Multidiciplinary Engineering Science and Technology (JMEST) ISSN: 59- Vol. Iue, January - 5 Advanced D-Partitioning Analyi and it Comparion with the haritonov Theorem Aement amen M. Yanev Profeor,

More information

Lecture 8 - SISO Loop Design

Lecture 8 - SISO Loop Design Lecture 8 - SISO Loop Deign Deign approache, given pec Loophaping: in-band and out-of-band pec Fundamental deign limitation for the loop Gorinevky Control Engineering 8-1 Modern Control Theory Appy reult

More information

Stability regions in controller parameter space of DC motor speed control system with communication delays

Stability regions in controller parameter space of DC motor speed control system with communication delays Stability region in controller parameter pace of DC motor peed control ytem with communication delay Şahin Sönmez, Saffet Ayaun Department of Electrical and Electronic Engineering, Nigde Univerity, 5124,

More information

Given the following circuit with unknown initial capacitor voltage v(0): X(s) Immediately, we know that the transfer function H(s) is

Given the following circuit with unknown initial capacitor voltage v(0): X(s) Immediately, we know that the transfer function H(s) is EE 4G Note: Chapter 6 Intructor: Cheung More about ZSR and ZIR. Finding unknown initial condition: Given the following circuit with unknown initial capacitor voltage v0: F v0/ / Input xt 0Ω Output yt -

More information

ME 375 FINAL EXAM SOLUTIONS Friday December 17, 2004

ME 375 FINAL EXAM SOLUTIONS Friday December 17, 2004 ME 375 FINAL EXAM SOLUTIONS Friday December 7, 004 Diviion Adam 0:30 / Yao :30 (circle one) Name Intruction () Thi i a cloed book eamination, but you are allowed three 8.5 crib heet. () You have two hour

More information

Pusan National University

Pusan National University Chapter 12. DESIGN VIA STATE SPACE Puan National Univerity oratory Table of Content v v v v v v v v Introduction Controller Deign Controllability Alternative Approache to Controller Deign Oberver Deign

More information

Automatic Control Systems. Part III: Root Locus Technique

Automatic Control Systems. Part III: Root Locus Technique www.pdhcenter.com PDH Coure E40 www.pdhonline.org Automatic Control Sytem Part III: Root Locu Technique By Shih-Min Hu, Ph.D., P.E. Page of 30 www.pdhcenter.com PDH Coure E40 www.pdhonline.org VI. Root

More information

1 Routh Array: 15 points

1 Routh Array: 15 points EE C28 / ME34 Problem Set 3 Solution Fall 2 Routh Array: 5 point Conider the ytem below, with D() k(+), w(t), G() +2, and H y() 2 ++2 2(+). Find the cloed loop tranfer function Y () R(), and range of k

More information

HOMEWORK ASSIGNMENT #2

HOMEWORK ASSIGNMENT #2 Texa A&M Univerity Electrical Engineering Department ELEN Integrated Active Filter Deign Methodologie Alberto Valde-Garcia TAMU ID# 000 17 September 0, 001 HOMEWORK ASSIGNMENT # PROBLEM 1 Obtain at leat

More information

G(s) = 1 s by hand for! = 1, 2, 5, 10, 20, 50, and 100 rad/sec.

G(s) = 1 s by hand for! = 1, 2, 5, 10, 20, 50, and 100 rad/sec. 6003 where A = jg(j!)j ; = tan Im [G(j!)] Re [G(j!)] = \G(j!) 2. (a) Calculate the magnitude and phae of G() = + 0 by hand for! =, 2, 5, 0, 20, 50, and 00 rad/ec. (b) ketch the aymptote for G() according

More information

Stochastic Optimization with Inequality Constraints Using Simultaneous Perturbations and Penalty Functions

Stochastic Optimization with Inequality Constraints Using Simultaneous Perturbations and Penalty Functions Stochatic Optimization with Inequality Contraint Uing Simultaneou Perturbation and Penalty Function I-Jeng Wang* and Jame C. Spall** The John Hopkin Univerity Applied Phyic Laboratory 11100 John Hopkin

More information

A PLC BASED MIMO PID CONTROLLER FOR MULTIVARIABLE INDUSTRIAL PROCESSES

A PLC BASED MIMO PID CONTROLLER FOR MULTIVARIABLE INDUSTRIAL PROCESSES ABCM Sympoium Serie in Mechatronic - Vol. 3 - pp.87-96 Copyright c 8 by ABCM A PLC BASE MIMO PI CONOLLE FO MULIVAIABLE INUSIAL POCESSES Joé Maria Galvez, jmgalvez@ufmg.br epartment of Mechanical Engineering

More information

Adaptive Control of Level in Water Tank: Simulation Study

Adaptive Control of Level in Water Tank: Simulation Study Adaptive Control of Level in Water Tank: Simulation Study Jiri Vojteek and Petr Dotal Abtract An adaptive control i a popular, o called modern control method which could be ued for variou type of ytem

More information

CONTROL SYSTEMS. Chapter 2 : Block Diagram & Signal Flow Graphs GATE Objective & Numerical Type Questions

CONTROL SYSTEMS. Chapter 2 : Block Diagram & Signal Flow Graphs GATE Objective & Numerical Type Questions ONTOL SYSTEMS hapter : Bloc Diagram & Signal Flow Graph GATE Objective & Numerical Type Quetion Quetion 6 [Practice Boo] [GATE E 994 IIT-Kharagpur : 5 Mar] educe the ignal flow graph hown in figure below,

More information

Chapter 10. Closed-Loop Control Systems

Chapter 10. Closed-Loop Control Systems hapter 0 loed-loop ontrol Sytem ontrol Diagram of a Typical ontrol Loop Actuator Sytem F F 2 T T 2 ontroller T Senor Sytem T TT omponent and Signal of a Typical ontrol Loop F F 2 T Air 3-5 pig 4-20 ma

More information

OBSERVER-BASED REDUCED ORDER CONTROLLER DESIGN FOR THE STABILIZATION OF LARGE SCALE LINEAR DISCRETE-TIME CONTROL SYSTEMS

OBSERVER-BASED REDUCED ORDER CONTROLLER DESIGN FOR THE STABILIZATION OF LARGE SCALE LINEAR DISCRETE-TIME CONTROL SYSTEMS International Journal o Computer Science, Engineering and Inormation Technology (IJCSEIT, Vol.1, No.5, December 2011 OBSERVER-BASED REDUCED ORDER CONTROLLER DESIGN FOR THE STABILIZATION OF LARGE SCALE

More information

1 Parity. 2 Time reversal. Even. Odd. Symmetry Lecture 9

1 Parity. 2 Time reversal. Even. Odd. Symmetry Lecture 9 Even Odd Symmetry Lecture 9 1 Parity The normal mode of a tring have either even or odd ymmetry. Thi alo occur for tationary tate in Quantum Mechanic. The tranformation i called partiy. We previouly found

More information

H DESIGN OF ROTOR FLUX ORIENTED CONTROLLED INDUCTION

H DESIGN OF ROTOR FLUX ORIENTED CONTROLLED INDUCTION H DESIGN OF ROTOR FLUX ORIENTED CONTROLLED INDUCTION MOTOR DRIVES: SPEED CONTROL, STABILITY ROBUSTNESS AND NOISE ATTENUATION João C. Bailio,, Joé A. Silva Jr.,, Jr., and Lui G. B. Rolim, Member, IEEE,

More information

Analysis of Step Response, Impulse and Ramp Response in the Continuous Stirred Tank Reactor System

Analysis of Step Response, Impulse and Ramp Response in the Continuous Stirred Tank Reactor System ISSN: 454-50 Volume 0 - Iue 05 May 07 PP. 7-78 Analyi of Step Repone, Impule and Ramp Repone in the ontinuou Stirred Tank Reactor Sytem * Zohreh Khohraftar, Pirouz Derakhhi, (Department of hemitry, Science

More information

Trajectory Planning and Feedforward Design for High Performance Motion Systems

Trajectory Planning and Feedforward Design for High Performance Motion Systems Trajectory Planning and Feedforward Deign for High Performance Motion Sytem Paul Lambrecht, Matthij Boerlage, Maarten Steinbuch Faculty of Mechanical Engineering, Control Sytem Technology Group Eindhoven

More information

Bogoliubov Transformation in Classical Mechanics

Bogoliubov Transformation in Classical Mechanics Bogoliubov Tranformation in Claical Mechanic Canonical Tranformation Suppoe we have a et of complex canonical variable, {a j }, and would like to conider another et of variable, {b }, b b ({a j }). How

More information

5. NON-LINER BLOCKS Non-linear standard blocks

5. NON-LINER BLOCKS Non-linear standard blocks 5. NON-LINER BLOCKS In previou chapter continuou tem or tem where to the change of the input a change of the output correponded, which in the whole range of the ignal value could be expreed b one equation,

More information

STATE RETENTION OF AN INVERTED PENDULUM

STATE RETENTION OF AN INVERTED PENDULUM ISSN:9-69 Potluri Krihna Murthy et al, Int.J.Computer echnology & Application,Vol 7 (,6-67 SAE REENION OF AN INVERED PENDULUM Potluri Krihna Murthy Aitant Profeor Department of Electrical and Electronic

More information

SKEE 3143 CONTROL SYSTEM DESIGN. CHAPTER 3 Compensator Design Using the Bode Plot

SKEE 3143 CONTROL SYSTEM DESIGN. CHAPTER 3 Compensator Design Using the Bode Plot SKEE 3143 CONTROL SYSTEM DESIGN CHAPTER 3 Compenator Deign Uing the Bode Plot 1 Chapter Outline 3.1 Introduc4on Re- viit to Frequency Repone, ploang frequency repone, bode plot tability analyi. 3.2 Gain

More information

Chapter 9: Controller design. Controller design. Controller design

Chapter 9: Controller design. Controller design. Controller design Chapter 9. Controller Deign 9.. Introduction 9.2. Eect o negative eedback on the network traner unction 9.2.. Feedback reduce the traner unction rom diturbance to the output 9.2.2. Feedback caue the traner

More information

NON-LINEAR SYSTEM CONTROL

NON-LINEAR SYSTEM CONTROL Non-linear Proce Control NON-LINEAR SYSTEM CONTROL. Introduction In practice, all phyical procee exhibit ome non-linear behaviour. Furthermore, when a proce how trong non-linear behaviour, a linear model

More information

Singular Value Analysis of Linear- Quadratic Systems!

Singular Value Analysis of Linear- Quadratic Systems! Singular Value Analyi of Linear- Quadratic Sytem! Robert Stengel! Optimal Control and Etimation MAE 546! Princeton Univerity, 2017!! Multivariable Nyquit Stability Criterion!! Matrix Norm and Singular

More information

Lecture 5 Introduction to control

Lecture 5 Introduction to control Lecture 5 Introduction to control Tranfer function reviited (Laplace tranform notation: ~jω) () i the Laplace tranform of v(t). Some rule: ) Proportionality: ()/ in () 0log log() v (t) *v in (t) () * in

More information

Implied Historical Federal Reserve Bank Behavior Under Uncertainty

Implied Historical Federal Reserve Bank Behavior Under Uncertainty Proceeding of the 2009 IEEE International Conference on Sytem, Man, and Cybernetic San Antonio, TX, USA - October 2009 Implied Hitorical Federal Reerve Bank Behavior Under Uncertainty Muhittin Yilmaz,

More information

5.5 Application of Frequency Response: Signal Filters

5.5 Application of Frequency Response: Signal Filters 44 Dynamic Sytem Second order lowpa filter having tranfer function H()=H ()H () u H () H () y Firt order lowpa filter Figure 5.5: Contruction of a econd order low-pa filter by combining two firt order

More information

Optimal Coordination of Samples in Business Surveys

Optimal Coordination of Samples in Business Surveys Paper preented at the ICES-III, June 8-, 007, Montreal, Quebec, Canada Optimal Coordination of Sample in Buine Survey enka Mach, Ioana Şchiopu-Kratina, Philip T Rei, Jean-Marc Fillion Statitic Canada New

More information

Efficient Methods of Doppler Processing for Coexisting Land and Weather Clutter

Efficient Methods of Doppler Processing for Coexisting Land and Weather Clutter Efficient Method of Doppler Proceing for Coexiting Land and Weather Clutter Ça gatay Candan and A Özgür Yılmaz Middle Eat Technical Univerity METU) Ankara, Turkey ccandan@metuedutr, aoyilmaz@metuedutr

More information

On the Robustness of the Characteristics Related to (M\M\1) ( \FCFS) Queue System Model

On the Robustness of the Characteristics Related to (M\M\1) ( \FCFS) Queue System Model www.ijemr.net ISSN (ONINE): 5-758, ISSN (PRINT): 394-696 Volume-5, Iue-3, June 5 International Journal of Engineering and Management Reearch Page Number: 839-847 On the Robutne of the haracteritic Related

More information