Chapter 6 Control Systems Design by Root-Locus Method. Lag-Lead Compensation. Lag lead Compensation Techniques Based on the Root-Locus Approach.
|
|
- Rosalind Robinson
- 6 years ago
- Views:
Transcription
1 hapter 6 ontrol Sytem Deign by Root-Lou Method Lag-Lead ompenation Lag lead ompenation ehnique Baed on the Root-Lou Approah. γ β K, ( γ >, β > ) In deigning lag lead ompenator, we onider two ae where γ βand γ β ae I γ β. In thi ae, the deign proe i a ombination of the deign of the lead ompenator and that of the lag ompenator. he deign proedure for the lag lead ompenator follow: Lag lead ompenation ehnique Baed on the Root-Lou Approah.. From the given performane peifiation, determine the deired loation for the dominant loed-loop pole.. Uing the unompenated open-loop tranfer funtion (), determine the angle defiieny φ if the dominant loed-loop pole are to be at the deired loation. he phae-lead portion of the lag lead ompenator mut ontribute thi angle φ. 3. Auming that we later hooe uffiiently large o that the magnitude of the lag portion β 3 Lag lead ompenation ehnique Baed on the Root-Lou Approah.
2 Lag lead ompenation ehnique Baed on the Root-Lou Approah. Lag lead ompenation ehnique Baed on the Root-Lou Approah. hooe the value of uh that where K and γ are already determined in tep 3. Hene, given the value of K v the value of β an be determined from thi lat equation. hen, uing the value of β thu determined, 6 Lag lead ompenation ehnique Baed on the Root-Lou Approah. Lag lead ompenation ehnique Baed on the Root-Lou Approah. 7 8
3 Lag lead ompenation ehnique Baed on the Root-Lou Approah. Example: Lag-Lead ompenator ae: γ β 9 R ( ) + ( ) he loed-loop tranfer funtion 0. ( ) ; ζ 0.; ω 0. + n rad e 0 Example: Lag-Lead ompenator ae: γ β Example: Lag-Lead ompenator ae: γ β he dominant loed-loop pole are It i deired ytem of the dominant loed-loop pole, 0. ± j.983 ζ 0. ω n rad e he damping ratio ζ 0. he undamped natural frequeny ω n rad e he tati veloity error ontant i 8 e - K v 80 - e We ue a lag-lead ompenator having the tranfer funtion γ β K, ( γ >, β > ) 3
4 z lead Example: Lag-Lead ompenator ae: γ β p lead 0. A B + K 0 ( 0.),. ± j.33 Example: Lag-Lead ompenator ae: γ β hu, the phae lead portion of the lag-lead ompenator beome K K γ 0. θ AB. 33 tan 60 B B B. 3 where, γ 0. 0 Example: Lag-Lead ompenator ae: γ β Example: Lag-Lead ompenator ae: γ β Next we determine the value of K K K ( 0.) ( ) ( 0.) A A A 3 B.+ j A3 A A B + K 0 ( 0.) hu K γ K A A A 3 B 6. 6
5 Example: Lag-Lead ompenator ae: γ β Example: Lag-Lead ompenator ae: γ β Firt the value of β i determined to atify the requirement on the tati veloity error ontant: K v lim 0 Hene, β i determined a lim K () 0 ( 0.) β γ β Kv lim ( 6.).008β β.97 7 Finally, we hooe the value of large enough o that and We may hooe.97.+ j.33 <.97 <.+ j Example: Lag-Lead ompenator Now the tranfer funtion of the deign lag-lead ompenator i given by 0. () Example: Lag-Lead ompenator he new damping ratio i ζ0.9 he ompenated ytem will have the open-loop tranfer funtion () ( 0. ) 9 New loed-loop pole are loated at -.±j.7 0
6 Example: Lag-Lead ompenator Example : Lag-Lead ompenator ae: γ β 0. ( ) he loed-loop tranfer funtion R ( ) + ( ) ; ζ 0.; ω 0. + n rad e Example : Lag-Lead ompenator ae: γ β It i deired ytem of the dominant loed-loop pole ζ 0. ω n rad e Example : Lag-Lead ompenator ae: γ β z lead. + K ( 0.) p 8.6 lead A 0,. ± j.33 K v 80 - e We ue a lag-lead ompenator having the tranfer funtion β β K, ( β > ) 3 θ B AB. 33 tan 3. B B B 6. 6
7 Example : Lag-Lead ompenator ae: γ β Example : Lag-Lead ompenator ae: γ β he phae lead portion of the lag-lead network thu beome z lead p lead. 0. β 8.6 β 3.6 For the phae lag portion, we may hooe 0 zlag 0. p lag β Sine the requirement on the tati veloity error ontant i 80 e -, We have K lim v 0 0. lim K 8K 80 K 0 0 hu, the lag-lead ompenator beome Example : Lag-Lead ompenator ae: γ β Example : Lag-Lead ompenator ae: γ β he ompenated ytem will have the open-loop tranfer funtion R ( ) ( ) ( ) he loed-loop tranfer funtion ( + 0.) ( ) New loed-loop pole and zero are loated at p 3.968; p 0.00; p3,.307 ± j.9 ( ) + ( ) ( + )( + )( + ) lim E lim lim z.; z 0. e he teady-tate error of the ytem for a unit-ramp input i he tati veloity error ontant, K v i define by Kv 77.6 e e
8 Example : Lag-Lead ompenator ae: γ β Example : Lag-Lead ompenator ae: γ β
Lag-Lead Compensator Design
Lag-Lead Compenator Deign ELEC 3 Spring 08 Lag or Lead Struture A bai ompenator onit of a gain, one real pole and one real zero Two type: phae-lead and phae-lag Phae-lead: provide poitive phae hift and
More informationCompensation Techniques
D Compenation ehnique Performane peifiation for the loed-loop ytem Stability ranient repone Æ, M (ettling time, overhoot) or phae and gain margin Steady-tate repone Æ e (teady tate error) rial and error
More information376 CHAPTER 6. THE FREQUENCY-RESPONSE DESIGN METHOD. D(s) = we get the compensated system with :
376 CHAPTER 6. THE FREQUENCY-RESPONSE DESIGN METHOD Therefore by applying the lead compenator with ome gain adjutment : D() =.12 4.5 +1 9 +1 we get the compenated ytem with : PM =65, ω c = 22 rad/ec, o
More informationControl 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 informationRoot 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 informationME 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 informationCOMM 602: Digital Signal Processing. Lecture 8. Digital Filter Design
COMM 60: Digital Signal Proeing Leture 8 Digital Filter Deign Remember: Filter Type Filter Band Pratial Filter peifiation Pratial Filter peifiation H ellipti H Pratial Filter peifiation p p IIR Filter
More informationLecture 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 informationHomework 12 Solution - AME30315, Spring 2013
Homework 2 Solution - AME335, Spring 23 Problem :[2 pt] The Aerotech AGS 5 i a linear motor driven XY poitioning ytem (ee attached product heet). A friend of mine, through careful experimentation, identified
More informationChapter 4. Simulations. 4.1 Introduction
Chapter 4 Simulation 4.1 Introdution In the previou hapter, a methodology ha been developed that will be ued to perform the ontrol needed for atuator haraterization. A tudy uing thi methodology allowed
More informationHomework Assignment No. 3 - Solutions
ECE 6440 Summer 2003 Page 1 Homework Aignment o. 3 Problem 1 (10 point) Aume an LPLL ha F() 1 and the PLL parameter are 0.8V/radian, K o 100 MHz/V, and the ocillation frequency, f oc 500MHz. Sketch the
More informationSKEE 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 informationPID CONTROL. Presentation kindly provided by Dr Andy Clegg. Advanced Control Technology Consortium (ACTC)
PID CONTROL Preentation kindly provided by Dr Andy Clegg Advaned Control Tehnology Conortium (ACTC) Preentation Overview Introdution PID parameteriation and truture Effet of PID term Proportional, Integral
More informationMODERN 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 information1 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 informationDigital 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 informationECE-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 informationToday s Lecture. Block Diagrams. Block Diagrams: Examples. Block Diagrams: Examples. Closed Loop System 06/03/2017
06/0/07 UW Britol Indutrial ontrol UFMF6W-0- ontrol Sytem ngineering UFMUY-0- Lecture 5: Block Diagram and Steady State rror Today Lecture Block diagram to repreent control ytem Block diagram manipulation
More informationME 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 informationEE/ME/AE324: Dynamical Systems. Chapter 8: Transfer Function Analysis
EE/ME/AE34: Dynamical Sytem Chapter 8: Tranfer Function Analyi The Sytem Tranfer Function Conider the ytem decribed by the nth-order I/O eqn.: ( n) ( n 1) ( m) y + a y + + a y = b u + + bu n 1 0 m 0 Taking
More information6.447 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 informationEE105 - Fall 2005 Microelectronic Devices and Circuits
EE5 - Fall 5 Microelectronic Device and ircuit Lecture 9 Second-Order ircuit Amplifier Frequency Repone Announcement Homework 8 due tomorrow noon Lab 7 next week Reading: hapter.,.3. Lecture Material Lat
More informationFigure 1: Unity Feedback System
MEM 355 Sample Midterm Problem Stability 1 a) I the following ytem table? Solution: G() = Pole: -1, -2, -2, -1.5000 + 1.3229i, -1.5000-1.3229i 1 ( + 1)( 2 + 3 + 4)( + 2) 2 A you can ee, all pole are on
More informationThe Skeldar V-150 flight control system. Modeling, identification and control of an unmanned helicopter. Saab AB. Saab Aerosystems.
The Skeldar V-5 flight ontrol ytem Modeling, identifiation and ontrol of an unmanned heliopter Ola Härkegård LiTH, November 8, 27 Organization Saab AB Saab Aeroytem Aeronauti Flight Control Sytem Aerodynami
More informationTHE SOLAR SYSTEM. We begin with an inertial system and locate the planet and the sun with respect to it. Then. F m. Then
THE SOLAR SYSTEM We now want to apply what we have learned to the olar ytem. Hitorially thi wa the great teting ground for mehani and provided ome of it greatet triumph, uh a the diovery of the outer planet.
More informationRoot 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 informationUVa Course on Physics of Particle Accelerators
UVa Coure on Phyi of Partile Aelerator B. Norum Univerity of Virginia G. A. Krafft Jefferon Lab 3/7/6 Leture x dx d () () Peudoharmoni Solution = give β β β () ( o µ + α in µ ) β () () β x dx ( + α() α
More informationFeedback Control Systems (FCS)
Feedback Control Sytem (FCS) Lecture19-20 Routh-Herwitz Stability Criterion Dr. Imtiaz Huain email: imtiaz.huain@faculty.muet.edu.pk URL :http://imtiazhuainkalwar.weebly.com/ Stability of Higher Order
More informationChapter #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 informationAnalysis 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 informationDelhi Noida Bhopal Hyderabad Jaipur Lucknow Indore Pune Bhubaneswar Kolkata Patna Web: Ph:
Serial :. PT_EE_A+C_Control Sytem_798 Delhi Noida Bhopal Hyderabad Jaipur Lucknow Indore Pune Bhubanewar olkata Patna Web: E-mail: info@madeeay.in Ph: -4546 CLASS TEST 8-9 ELECTRICAL ENGINEERING Subject
More informationModule 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 informationCHAPTER 4 DESIGN OF STATE FEEDBACK CONTROLLERS AND STATE OBSERVERS USING REDUCED ORDER MODEL
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
More informationChapter 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 informationModeling and Simulation of Buck-Boost Converter with Voltage Feedback Control
MATE Web of onferene 3, 0006 ( 05) DOI: 0.05/ mateonf/ 053 0006 Owned by the author, publihed by EDP Siene, 05 Modeling and Simulation of BukBoot onverter with oltage Feedbak ontrol Xuelian Zhou, Qiang
More informationEE 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 informationCALIFORNIA 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 informationApplication of Fuzzy C-Means Clustering in Power System Model Reduction for Controller Design
Proeeding of the 5th WSEAS Int. Conf. on COMPUAIONAL INELLIGENCE, MAN-MACHINE SYSEMS AND CYBERNEICS, Venie, Italy, November 20-22, 2006 223 Appliation of Fuzzy C-Mean Clutering in Power Sytem Model Redution
More informationQuestion 1 Equivalent Circuits
MAE 40 inear ircuit Fall 2007 Final Intruction ) Thi exam i open book You may ue whatever written material you chooe, including your cla note and textbook You may ue a hand calculator with no communication
More informationAnalysis of Stability &
INC 34 Feedback Control Sytem Analyi of Stability & Steady-State Error S Wonga arawan.won@kmutt.ac.th Summary from previou cla Firt-order & econd order ytem repone τ ωn ζω ω n n.8.6.4. ζ ζ. ζ.5 ζ ζ.5 ct.8.6.4...4.6.8..4.6.8
More informationLecture 16. Kinetics and Mass Transfer in Crystallization
Leture 16. Kineti and Ma Tranfer in Crytallization Crytallization Kineti Superaturation Nuleation - Primary nuleation - Seondary nuleation Crytal Growth - Diffuion-reation theory - Srew-diloation theory
More informationCHAPTER 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 information6.302 Feedback Systems Recitation 6: Steady-State Errors Prof. Joel L. Dawson S -
6302 Feedback ytem Recitation 6: teadytate Error Prof Joel L Dawon A valid performance metric for any control ytem center around the final error when the ytem reache teadytate That i, after all initial
More informationGiven 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 informationInverse Kinematics 1 1/21/2018
Invere Kinemati 1 Invere Kinemati 2 given the poe of the end effetor, find the joint variable that produe the end effetor poe for a -joint robot, given find 1 o R T 3 2 1,,,,, q q q q q q RPP + Spherial
More informationChapter 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 informationDesign 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 informationCONTROL 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 informationSidelobe-Suppression Technique Applied To Binary Phase Barker Codes
Journal of Engineering and Development, Vol. 16, No.4, De. 01 ISSN 1813-78 Sidelobe-Suppreion Tehnique Applied To Binary Phae Barker Code Aitant Profeor Dr. Imail M. Jaber Al-Mutaniriya Univerity College
More informationFunction 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 informationChapter 8. Root Locus Techniques
Chapter 8 Rt Lcu Technique Intrductin Sytem perfrmance and tability dt determined dby cled-lp l ple Typical cled-lp feedback cntrl ytem G Open-lp TF KG H Zer -, - Ple 0, -, -4 K 4 Lcatin f ple eaily fund
More informationAccelerator Physics. G. A. Krafft Jefferson Lab Old Dominion University Lecture 7
Aeerator Phyi G. A. Krafft Jefferon Lab Od Dominion Univerity Leture 7 ODU Aeerator Phyi Spring 05 Soution to Hi Equation in Ampitude-Phae form To get a more genera expreion for the phae advane, onider
More informationControl 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 informationECE382/ME482 Spring 2004 Homework 4 Solution November 14,
ECE382/ME482 Spring 2004 Homework 4 Solution November 14, 2005 1 Solution to HW4 AP4.3 Intead of a contant or tep reference input, we are given, in thi problem, a more complicated reference path, r(t)
More informationLecture 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 informationSolutions. 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 informationModeling, Analysis and Simulation of Robust Control Strategy on a 10kVA STATCOM for Reactive Power Compensation
International Journal of Eletrial Engineering. ISSN 0974-58 Volume 4, Number (0), pp. 6-8 International Reearh Publiation Houe http://www.irphoue.om Modeling, Analyi and Simulation of Robut Control Strategy
More informationState-space feedback 5 Tutorial examples and use of MATLAB
State-pace feedback 5 Tutorial example and ue of MTLB J Roiter Introduction The previou video howed how tate feedback can place pole preciely a long a the ytem u fully controllable. x u x Kx Bu Thi video
More information@(; t) p(;,b t) +; t), (; t)) (( whih lat line follow from denition partial derivative. in relation quoted in leture. Th derive wave equation for ound
24 Spring 99 Problem Set 5 Optional Problem Phy February 23, 999 Handout Derivation Wave Equation for Sound. one-dimenional wave equation for ound. Make ame ort Derive implifying aumption made in deriving
More informationHomework #7 Solution. Solutions: ΔP L Δω. Fig. 1
Homework #7 Solution Aignment:. through.6 Bergen & Vittal. M Solution: Modified Equation.6 becaue gen. peed not fed back * M (.0rad / MW ec)(00mw) rad /ec peed ( ) (60) 9.55r. p. m. 3600 ( 9.55) 3590.45r.
More informationStability Criterion Routh Hurwitz
EES404 Fundamental of Control Sytem Stability Criterion Routh Hurwitz DR. Ir. Wahidin Wahab M.Sc. Ir. Arie Subiantoro M.Sc. Stability A ytem i table if for a finite input the output i imilarly finite A
More informationME 375 EXAM #1 Tuesday February 21, 2006
ME 375 EXAM #1 Tueday February 1, 006 Diviion Adam 11:30 / Savran :30 (circle one) Name Intruction (1) Thi i a cloed book examination, but you are allowed one 8.5x11 crib heet. () You have one hour to
More informationLecture 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 informationStability. 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 informationAnalysis of Feedback Control Systems
Colorado Shool of Mine CHEN403 Feedbak Control Sytem Analyi of Feedbak Control Sytem ntrodution to Feedbak Control Sytem 1 Cloed oo Reone 3 Breaking Aart the Problem to Calulate the Overall Tranfer Funtion
More informationECE 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 informationDepartment of Mechanical Engineering Massachusetts Institute of Technology Modeling, Dynamics and Control III Spring 2002
Department of Mechanical Engineering Maachuett Intitute of Technology 2.010 Modeling, Dynamic and Control III Spring 2002 SOLUTIONS: Problem Set # 10 Problem 1 Etimating tranfer function from Bode Plot.
More informationThe Root Locus Method
The Root Locu Method MEM 355 Performance Enhancement of Dynamical Sytem Harry G. Kwatny Department of Mechanical Engineering & Mechanic Drexel Univerity Outline The root locu method wa introduced by Evan
More informationAli Karimpour Associate Professor Ferdowsi University of Mashhad
LINEAR CONTROL SYSTEMS Ali Karimour Aoiate Profeor Ferdowi Univerity of Mahhad Leture 0 Leture 0 Frequeny domain hart Toi to be overed inlude: Relative tability meaure for minimum hae ytem. ain margin.
More informationControl Systems. Control Systems Design Lead-Lag Compensator.
Design Lead-Lag Compensator hibum@seoulteh.a.kr Outline Lead ompensator design in frequeny domain Lead ompensator design steps. Example on lead ompensator design. Frequeny Domain Design Frequeny response
More informationMM1: 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( ) 2. 1) Bode plots/transfer functions. a. Draw magnitude and phase bode plots for the transfer function
ECSE CP7 olution Spring 5 ) Bode plot/tranfer function a. Draw magnitude and phae bode plot for the tranfer function H( ). ( ) ( E4) In your magnitude plot, indicate correction at the pole and zero. Step
More informationCISE302: Linear Control Systems
Term 8 CISE: Linear Control Sytem Dr. Samir Al-Amer Chapter 7: Root locu CISE_ch 7 Al-Amer8 ١ Learning Objective Undertand the concept of root locu and it role in control ytem deign Be able to ketch root
More informationECE-320 Linear Control Systems. Winter 2013, Exam 1. No calculators or computers allowed, you may leave your answers as fractions.
ECE-320 Linear Control Systems Winter 2013, Exam 1 No alulators or omputers allowed, you may leave your answers as frations. All problems are worth 3 points unless noted otherwise. Total /100 1 Problems
More informationControl Engineering An introduction with the use of Matlab
Derek Atherton An introdution with the ue of Matlab : An introdution with the ue of Matlab nd edition 3 Derek Atherton ISBN 978-87-43-473- 3 Content Content Prefae 9 About the author Introdution What i?
More informationLecture 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 informationEGN 3353C Fluid Mechanics
eture 5 Bukingham PI Theorem Reall dynami imilarity beteen a model and a rototye require that all dimenionle variable mut math. Ho do e determine the '? Ue the method of reeating variable 6 te Ste : Parameter
More informationG(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 informationLecture 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 informationThe Prime Number Theorem
he Prime Number heorem Yuuf Chebao he main purpoe of thee note i to preent a fairly readable verion of a proof of the Prime Number heorem (PN, epanded from Setion 7-8 of Davenport tet [3]. We intend to
More informationHigh-Speed Serial Interface Circuits and Systems. Lect. 4 Phase-Locked Loop (PLL) Type 1 (Chap. 8 in Razavi)
High-Speed Serial Iterface Circuit ad Sytem Lect. 4 Phae-Locked Loop (PLL) Type 1 (Chap. 8 i Razavi) PLL Phae lockig loop A (egative-feedback) cotrol ytem that geerate a output igal whoe phae (ad frequecy)
More informationHomework 7 Solution - AME 30315, Spring s 2 + 2s (s 2 + 2s + 4)(s + 20)
1 Homework 7 Solution - AME 30315, Spring 2015 Problem 1 [10/10 pt] Ue partial fraction expanion to compute x(t) when X 1 () = 4 2 + 2 + 4 Ue partial fraction expanion to compute x(t) when X 2 () = ( )
More informationInternal Model Control
Internal Model Control Part o a et o leture note on Introdution to Robut Control by Ming T. Tham 2002 The Internal Model Prinile The Internal Model Control hiloohy relie on the Internal Model Prinile,
More informationThe state variable description of an LTI system is given by 3 1O. Statement for Linked Answer Questions 3 and 4 :
CHAPTER 6 CONTROL SYSTEMS YEAR TO MARKS MCQ 6. The tate variable decription of an LTI ytem i given by Jxo N J a NJx N JN K O K OK O K O xo a x + u Kxo O K 3 a3 OKx O K 3 O L P L J PL P L P x N K O y _
More informationGain 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 informationChapter 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 informationAutomatic 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 informationELEC 372 LECTURE NOTES, WEEK 4 Dr. Amir G. Aghdam Concordia University
ELEC 37 LECTURE NOTES, WEE 4 Dr Amir G Aghdam Cocordia Uiverity Part of thee ote are adapted from the material i the followig referece: Moder Cotrol Sytem by Richard C Dorf ad Robert H Bihop, Pretice Hall
More informationExtending the Concept of Analog Butterworth Filter for Fractional Order Systems
Extending the Conept of Analog Butterworth Filter for Frational Order Sytem Anih Aharya a, Saptarhi Da b, Indranil Pan, and Shantanu Da d a) Department of Intrumentation and Eletroni Engineering, Jadavpur
More informationMEM 355 Performance Enhancement of Dynamical Systems Root Locus Analysis
MEM 355 Performance Enhancement of Dynamical Sytem Root Locu Analyi Harry G. Kwatny Department of Mechanical Engineering & Mechanic Drexel Univerity Outline The root locu method wa introduced by Evan in
More informationDeveloping Transfer Functions from Heat & Material Balances
Colorado Sool of Mine CHEN43 Stirred ank Heater Develoing ranfer untion from Heat & Material Balane Examle ranfer untion Stirred ank Heater,,, A,,,,, We will develo te tranfer funtion for a tirred tank
More informationChapter 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 informationLecture 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 informationLinear-Quadratic Control System Design
Linear-Quadratic Control Sytem Deign Robert Stengel Optimal Control and Etimation MAE 546 Princeton Univerity, 218! Control ytem configuration! Proportional-integral! Proportional-integral-filtering! Model
More informationThese are practice problems for the final exam. You should attempt all of them, but turn in only the even-numbered problems!
Math 33 - ODE Due: 7 December 208 Written Problem Set # 4 Thee are practice problem for the final exam. You hould attempt all of them, but turn in only the even-numbered problem! Exercie Solve the initial
More informationDesign of Digital Filters
Deign of Digital Filter Paley-Wiener Theorem [ ] ( ) If h n i a caual energy ignal, then ln H e dω< B where B i a finite upper bound. One implication of the Paley-Wiener theorem i that a tranfer function
More informationFRTN10 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 informationu(t) Figure 1. Open loop control system
Open loop conrol v cloed loop feedbac conrol The nex wo figure preen he rucure of open loop and feedbac conrol yem Figure how an open loop conrol yem whoe funcion i o caue he oupu y o follow he reference
More informationMassachusetts 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 informationR. W. Erickson. Department of Electrical, Computer, and Energy Engineering University of Colorado, Boulder
R. W. Erickon Department of Electrical, Computer, and Energy Engineering Univerity of Colorado, Boulder Cloed-loop buck converter example: Section 9.5.4 In ECEN 5797, we ued the CCM mall ignal model to
More information