Frequency (rad/s)

Similar documents
Homework 7 - Solutions

ELECTRONICS & COMMUNICATIONS DEP. 3rd YEAR, 2010/2011 CONTROL ENGINEERING SHEET 5 Lead-Lag Compensation Techniques

Systems Analysis and Control

AMME3500: System Dynamics & Control

CHAPTER 7 : BODE PLOTS AND GAIN ADJUSTMENTS COMPENSATION

ECE382/ME482 Spring 2005 Homework 7 Solution April 17, K(s + 0.2) s 2 (s + 2)(s + 5) G(s) =

Mechanical Systems Part A: State-Space Systems Lecture AL12

Transient response via gain adjustment. Consider a unity feedback system, where G(s) = 2. The closed loop transfer function is. s 2 + 2ζωs + ω 2 n

EE C128 / ME C134 Fall 2014 HW 8 - Solutions. HW 8 - Solutions

MAE 143B - Homework 9

Outline. Classical Control. Lecture 5

Systems Analysis and Control

Stability of CL System

Frequency Response Analysis

Module 5: Design of Sampled Data Control Systems Lecture Note 8

EE C128 / ME C134 Fall 2014 HW 6.2 Solutions. HW 6.2 Solutions

ME 475/591 Control Systems Final Exam Fall '99

VALLIAMMAI ENGINEERING COLLEGE SRM Nagar, Kattankulathur

Digital Control Systems

EE 4343/ Control System Design Project LECTURE 10

ECE382/ME482 Spring 2005 Homework 6 Solution April 17, (s/2 + 1) s(2s + 1)[(s/8) 2 + (s/20) + 1]

Frequency Response Techniques

Dynamic Compensation using root locus method

ECE 486 Control Systems

R a) Compare open loop and closed loop control systems. b) Clearly bring out, from basics, Force-current and Force-Voltage analogies.

(b) A unity feedback system is characterized by the transfer function. Design a suitable compensator to meet the following specifications:

Engraving Machine Example

Today (10/23/01) Today. Reading Assignment: 6.3. Gain/phase margin lead/lag compensator Ref. 6.4, 6.7, 6.10

NADAR SARASWATHI COLLEGE OF ENGINEERING AND TECHNOLOGY Vadapudupatti, Theni

ECE382/ME482 Spring 2005 Homework 8 Solution December 11,

6.1 Sketch the z-domain root locus and find the critical gain for the following systems K., the closed-loop characteristic equation is K + z 0.

] [ 200. ] 3 [ 10 4 s. [ ] s + 10 [ P = s [ 10 8 ] 3. s s (s 1)(s 2) series compensator ] 2. s command pre-filter [ 0.

H(s) = s. a 2. H eq (z) = z z. G(s) a 2. G(s) A B. s 2 s(s + a) 2 s(s a) G(s) 1 a 1 a. } = (z s 1)( z. e ) ) (z. (z 1)(z e at )(z e at )

Exercise 1 (A Non-minimum Phase System)

16.30/31, Fall 2010 Recitation # 2

Exercise 1 (A Non-minimum Phase System)

r + - FINAL June 12, 2012 MAE 143B Linear Control Prof. M. Krstic

Professor Fearing EE C128 / ME C134 Problem Set 7 Solution Fall 2010 Jansen Sheng and Wenjie Chen, UC Berkeley

DEPARTMENT OF ELECTRICAL AND ELECTRONICS ENGINEERING

Root Locus Methods. The root locus procedure

Outline. Classical Control. Lecture 1

EECS C128/ ME C134 Final Wed. Dec. 14, am. Closed book. One page, 2 sides of formula sheets. No calculators.

R10 JNTUWORLD B 1 M 1 K 2 M 2. f(t) Figure 1

LINEAR CONTROL SYSTEMS. Ali Karimpour Associate Professor Ferdowsi University of Mashhad

Control Systems. Control Systems Design Lead-Lag Compensator.

Design via Frequency Response

PM diagram of the Transfer Function and its use in the Design of Controllers

Problem Weight Score Total 100

Controls Problems for Qualifying Exam - Spring 2014

1 (s + 3)(s + 2)(s + a) G(s) = C(s) = K P + K I

= rad/sec. We can find the last parameter, T, from ωcg new

MAE 143B - Homework 8 Solutions

Procedure for sketching bode plots (mentioned on Oct 5 th notes, Pg. 20)

MASSACHUSETTS INSTITUTE OF TECHNOLOGY Department of Mechanical Engineering Dynamics and Control II Fall K(s +1)(s +2) G(s) =.

MASSACHUSETTS INSTITUTE OF TECHNOLOGY Department of Mechanical Engineering Dynamics and Control II Fall 2007

Control Systems. University Questions

The requirements of a plant may be expressed in terms of (a) settling time (b) damping ratio (c) peak overshoot --- in time domain

Delhi Noida Bhopal Hyderabad Jaipur Lucknow Indore Pune Bhubaneswar Kolkata Patna Web: Ph:

Frequency methods for the analysis of feedback systems. Lecture 6. Loop analysis of feedback systems. Nyquist approach to study stability

Lecture 14 - Using the MATLAB Control System Toolbox and Simulink Friday, February 8, 2013

MAE 143B - Homework 9

ECE 388 Automatic Control

KINGS COLLEGE OF ENGINEERING DEPARTMENT OF ELECTRONICS AND COMMUNICATION ENGINEERING

EECS C128/ ME C134 Final Wed. Dec. 15, am. Closed book. Two pages of formula sheets. No calculators.

EECS C128/ ME C134 Final Thu. May 14, pm. Closed book. One page, 2 sides of formula sheets. No calculators.

Boise State University Department of Electrical Engineering ECE461 Control Systems. Control System Design in the Frequency Domain

CONTROL SYSTEMS ENGINEERING Sixth Edition International Student Version

Design via Root Locus

MAS107 Control Theory Exam Solutions 2008

Exercises for lectures 13 Design using frequency methods

100 (s + 10) (s + 100) e 0.5s. s 100 (s + 10) (s + 100). G(s) =

Design via Root Locus

FREQUENCY-RESPONSE DESIGN

Loop shaping exercise

Übersetzungshilfe / Translation aid (English) To be returned at the end of the exam!

Automatic Control (MSc in Mechanical Engineering) Lecturer: Andrea Zanchettin Date: Student ID number... Signature...

INSTITUTE OF AERONAUTICAL ENGINEERING Dundigal, Hyderabad ELECTRICAL AND ELECTRONICS ENGINEERING TUTORIAL QUESTION BANK

CONTROL * ~ SYSTEMS ENGINEERING

Compensation 8. f4 that separate these regions of stability and instability. The characteristic S 0 L U T I 0 N S

a. Closed-loop system; b. equivalent transfer function Then the CLTF () T is s the poles of () T are s from a contribution of a

Classify a transfer function to see which order or ramp it can follow and with which expected error.

Problem 1 (Analysis of a Feedback System - Bode, Root Locus, Nyquist) Consider the feedback system defined by the open loop transfer function 1.

SAMPLE SOLUTION TO EXAM in MAS501 Control Systems 2 Autumn 2015

Chapter 6 - Solved Problems

INTRODUCTION TO DIGITAL CONTROL

9/9/2011 Classical Control 1

INSTITUTE OF AERONAUTICAL ENGINEERING (Autonomous) Dundigal, Hyderabad

Raktim Bhattacharya. . AERO 422: Active Controls for Aerospace Vehicles. Frequency Response-Design Method

Control Systems. EC / EE / IN. For

Root Locus Techniques

Positioning Servo Design Example

1 (20 pts) Nyquist Exercise

Automatic Control 2. Loop shaping. Prof. Alberto Bemporad. University of Trento. Academic year

APPLICATIONS FOR ROBOTICS

10ES-43 CONTROL SYSTEMS ( ECE A B&C Section) % of Portions covered Reference Cumulative Chapter. Topic to be covered. Part A

CYBER EXPLORATION LABORATORY EXPERIMENTS

Contents. PART I METHODS AND CONCEPTS 2. Transfer Function Approach Frequency Domain Representations... 42

ECSE 4962 Control Systems Design. A Brief Tutorial on Control Design

ESE319 Introduction to Microelectronics. Feedback Basics

8.1.6 Quadratic pole response: resonance

Transcription:

. The frequency response of the plant in a unity feedback control systems is shown in Figure. a) What is the static velocity error coefficient K v for the system? b) A lead compensator with a transfer function Ts G() s = K α Ts is introduced in the forward path with α = 0. and /T = 0 rads/s =. What gain K is required to obtain a crossover frequency ω c = 3.6 rads/s? c) With the lead compensator in place, a lag compensator with a transfer function Ts G() s = K β Ts is to be used to restore K v to its original value. What values of K and β are required? d) Place the pole of the lag compensator at 3.6 rads / s and sketch the compensated frequency response on the graph Figure. e) Determine approximately the gain and phase margins of the system with the lag/lead compensation. 0 0 0 0 Magnitude 0-0 - 0-3 0-4 0-5 0 0 0 0 0 3 Frequency (rad/s)

-50-00 -50 Phase (deg) -00-50 -300-350 -400 0 0 0 0 0 3 Frequency (rad/s) (a) Static velocity error coefficient K v By inspection, low-frequency response is of the form K v /s (amplitude-ratio slope = decade/decade; phase = 90º). At ω =, A(ω) = 00 K v = 00 s. (b) Lead compensator To make full use of the MATLAB tools, we should identify a transfer function model from the given plant frequency response. We can see amplitude-ratio slope changes of at 0 rad/s, and at 00 rad/s, with corresponding phase changes of 90º and 80º respectively. Hence we can infer that the transfer function is of the form 00 Gs () = s s s s + 0 + ς 00 00 The damping ratio can be found from the 'quality factor' Q = ς, which is the departure of the second-order factor from the asymptote at ω = ω n =00 rad/s: By inspection Q = 0.4/0. = ζ = 0.5. Hence, we can define the plant transfer function thus: G = tf(00, conv([/0 0], [/00^ *0.5/00 ])); G = zpk(g) Zero/pole/gain: 0000000 ----------------------------- s (s+0) (s^ + 50s e004)

We want to find the gain K of the lead compensator s /0+ G() s = K s /00 such that the unity-gain crossover frequency ω c = 3.6 rad/s. So, define the lead compensator with a gain of : G = tf([/0 ], [/00 ]) Transfer function: 0.05 s ---------- 0.0 s Invoke sisotool with G as the plant: sisotool(g) Let's customise the tool to suit the present problem: hide the root-locus tool (de-select Root Locus in the View menu), and select the Natural frequency format for the compensator (Compensators/Format ). Right click and select Grid. The design pane should now look like this: 3

Import the lead compensator G into the block C (File/Import ): Now, drag the magnitude plot down until the crossover frequency (displayed along with the Phase Margin on the phase plot) is 3.6 rad/s: The required compensator gain is displayed in the Current Compensator box: K = 0.303; (c) Lag compensator The Bode gain (and hence the velocity error coefficient) of the open-loop transfer function has been reduced by a factor K = 0.303. To restore it to the initial value of 00, the gain K of the lag compensator Ts G() s = K β Ts must be set to K = /K K = 3.3003 4

The high-frequency gain of the lag compensator is K /β. Hence, to restore the open-loop magnitude in the crossover region, we require K /β (approximate, because this is the asymptotic value, which may not apply exactly at the crossover frequency). So, we'll set β to this value and adjust the value later: beta = K beta = 3.3003 (d) Effect of lag compensator With the lag compensator pole at s = /βt = 3. 6 rad/s, we have T = /beta/3.6 T = 0.0959 and the transfer function of the lag compensator is G = tf(k*[t ], [beta*t ]); G = zpk(g) ; Zero/pole/gain: (s+0.43) --------- (s+3.6) To include the lag compensator in sisotool, we could import G*G into the block C or, alternatively, edit the compensator within sisotool: Click on the Current Compensator box, use the Add Real Zero and Add Real Pole buttons to locate the compensator pole and zero, and adjust the compensator gain to K K = : 5

Note that the crossover frequency has not been precisely recovered. We could drag the lag compensator zero (effectively adjusting β) until the frequency is displayed as 3.6 rad/s: K v = 00 ω c = 3.6 With the lag compensator pole at 3.6 rad/s and the zero adjusted to rad/s, the adjusted value of β is: beta = /3.6 beta = 3.480 (e) Stability margins The gain and phase margins can be read off directly as 5.54 db and 49º, respectively. In absolute ratio terms, GM = 0^(5.54/0) GM =.893 General comments It is instructive to look at the contributions of the lead and lag compensators to the overall open-loop transfer function: G = tf(k*[/0 ], [/00 ]); G = tf(k*[/ ], [/3.6 ]); bode(g, G*G, G*K*G*G), grid legend('g', 'G*G', 'G*G*G') 6

00 Bode Diagram 50 Magnitude (db) 0-50 -00-50 Phase (deg) -00-90 -80-70 G G*G G*G*G -360 0-0 0 0 0 0 3 0 4 Frequency (rad/sec) The blue curves show that if the feedback loop was closed with proportional control so as to give the desired K v = 00, the crossover frequency would be 47.8 rad/s and the phase margin would be only 5.5º. With the lead compensator (green curves), the phase was boosted in the desired crossover region (around 3.6 rad/s), but the loop gain had to be reduced to get gain crossover at this frequency. The resulting phase margin was a healthy 6.5º, but at the expense of reducing K v to 30.3 s. The lag compensator was introduced (red curves) to boost the low-frequency magnitude back to its previous level, while maintaining the crossover conditions. The lag compensator was positioned at sufficiently low frequencies so that its residual phase lag at the crossover frequency was quite small (about 3.5º), thereby not too seriously compromising the phase margin gained by using the lead compensator. 7