Feedback design for the Buck Converter

Similar documents
Chapter 9: Controller design

Lecture 50 Changing Closed Loop Dynamic Response with Feedback and Compensation

B. T(s) Modification Design Example 1. DC Conditions 2. Open Loop AC Conditions 3. Closed Loop Conditions

6.302 Feedback Systems

ECE1750, Spring Week 11 Power Electronics

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

ANALYSIS OF SMALL-SIGNAL MODEL OF A PWM DC-DC BUCK-BOOST CONVERTER IN CCM.

Regulated DC-DC Converter

Chapter 10 Feedback. PART C: Stability and Compensation

Studio 9 Review Operational Amplifier Stability Compensation Miller Effect Phase Margin Unity Gain Frequency Slew Rate Limiting Reading: Text sec 5.

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

Homework 7 - Solutions

The Approximating Impedance

ECE3050 Assignment 7

Automatic Control (TSRT15): Lecture 7

R. W. Erickson. Department of Electrical, Computer, and Energy Engineering University of Colorado, Boulder

Homework Assignment 11

Homework Assignment 08

Lecture 46 Bode Plots of Transfer Functions:II A. Low Q Approximation for Two Poles w o

DESIGN MICROELECTRONICS ELCT 703 (W17) LECTURE 3: OP-AMP CMOS CIRCUIT. Dr. Eman Azab Assistant Professor Office: C

Dynamic circuits: Frequency domain analysis

Operational Amplifiers

Switched-Capacitor Circuits David Johns and Ken Martin University of Toronto

FEEDBACK AND STABILITY

The output voltage is given by,

ELECTRONIC SYSTEMS. Basic operational amplifier circuits. Electronic Systems - C3 13/05/ DDC Storey 1

Converter System Modeling via MATLAB/Simulink

Electronic Circuits. Prof. Dr. Qiuting Huang Integrated Systems Laboratory

Chapter 8: Converter Transfer Functions

H(s) = 2(s+10)(s+100) (s+1)(s+1000)

Section 5 Dynamics and Control of DC-DC Converters

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

Laplace Transform Analysis of Signals and Systems

ECE2210 Final given: Spring 08

ECE137B Final Exam. There are 5 problems on this exam and you have 3 hours There are pages 1-19 in the exam: please make sure all are there.

ECE2210 Final given: Fall 13

ESE319 Introduction to Microelectronics. Feedback Basics

Steady State Frequency Response Using Bode Plots

Modeling Buck Converter by Using Fourier Analysis

Final Exam. 55:041 Electronic Circuits. The University of Iowa. Fall 2013.

Frequency Dependent Aspects of Op-amps

Estimation of Circuit Component Values in Buck Converter using Efficiency Curve

EE 3CL4: Introduction to Control Systems Lab 4: Lead Compensation

ECE Circuit Theory. Final Examination. December 5, 2008

ECEN 607 (ESS) Op-Amps Stability and Frequency Compensation Techniques. Analog & Mixed-Signal Center Texas A&M University

MAS107 Control Theory Exam Solutions 2008

ECE 3050A, Spring 2004 Page 1. FINAL EXAMINATION - SOLUTIONS (Average score = 78/100) R 2 = R 1 =

Lecture 17 Date:

Stability & Compensation

Index. Index. More information. in this web service Cambridge University Press

UNIVERSITY OF BOLTON SCHOOL OF ENGINEERING BENG (HONS) IN BIOMEDICAL ENGINEERING SEMESTER 1 EXAMINATION 2017/2018 ADVANCED BIOMECHATRONIC SYSTEMS

EE 321 Analog Electronics, Fall 2013 Homework #3 solution

KINGS COLLEGE OF ENGINEERING DEPARTMENT OF ELECTRONICS AND COMMUNICATION ENGINEERING

55:041 Electronic Circuits The University of Iowa Fall Final Exam

ENGN3227 Analogue Electronics. Problem Sets V1.0. Dr. Salman Durrani

Course Summary. The course cannot be summarized in one lecture.

R. W. Erickson. Department of Electrical, Computer, and Energy Engineering University of Colorado, Boulder

EEE 184 Project: Option 1

Lecture 47 Switch Mode Converter Transfer Functions: Tvd(s) and Tvg(s) A. Guesstimating Roots of Complex Polynomials( this section is optional)

Appendix A: Exercise Problems on Classical Feedback Control Theory (Chaps. 1 and 2)

Time Varying Circuit Analysis

Chapter 6 Frequency response of circuits. Stability

Stability and Frequency Compensation

ECE137B Final Exam. Wednesday 6/8/2016, 7:30-10:30PM.

First and Second Order Circuits. Claudio Talarico, Gonzaga University Spring 2015

Chapter 11 AC and DC Equivalent Circuit Modeling of the Discontinuous Conduction Mode

Application Report. Mixed Signal Products SLOA021

EXPERIMENT 07 TO STUDY DC RC CIRCUIT AND TRANSIENT PHENOMENA

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

Switched Capacitor: Sampled Data Systems

EE 422G - Signals and Systems Laboratory

Analysis and Design of Analog Integrated Circuits Lecture 12. Feedback

OPERATIONAL AMPLIFIER APPLICATIONS

Introducing Negative Feedback with an Integrator as the Central Element

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

ESE319 Introduction to Microelectronics. Feedback Basics

Dr Ian R. Manchester Dr Ian R. Manchester AMME 3500 : Review

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

E40M. Op Amps. M. Horowitz, J. Plummer, R. Howe 1

Conventional Paper-I-2011 PART-A

EECE 2510 Circuits and Signals, Biomedical Applications Final Exam Section 3. Name:

VALLIAMMAI ENGINEERING COLLEGE SRM Nagar, Kattankulathur

MAE143a: Signals & Systems (& Control) Final Exam (2011) solutions

Digital Control: Summary # 7

AN ENERGY BASED MINIMUM-TIME OPTIMAL CONTROL OF DC-DC CONVERTERS

IMPERIAL COLLEGE OF SCIENCE, TECHNOLOGY AND MEDICINE UNIVERSITY OF LONDON DEPARTMENT OF ELECTRICAL AND ELECTRONIC ENGINEERING EXAMINATIONS 2010

Unit 8: Part 2: PD, PID, and Feedback Compensation

AND8321/D. Compensation of a PFC Stage Driven by the NCP1654/5

Chapter 2. Classical Control System Design. Dutch Institute of Systems and Control

Conventional Paper-I Part A. 1. (a) Define intrinsic wave impedance for a medium and derive the equation for intrinsic vy

To investigate further the series LCR circuit, especially around the point of minimum impedance. 1 Electricity & Electronics Constructor EEC470

PHYS225 Lecture 9. Electronic Circuits

Systems Analysis and Control

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 )

U1 is zero based because its noninverting terminal is connected to circuit common. Therefore, the circuit reference voltage is 0 V.

Electronics II. Final Examination

2 nd Order PLL Design and Analysis

Impedance Interactions: An

LECTURE 8 Fundamental Models of Pulse-Width Modulated DC-DC Converters: f(d)

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

Transcription:

Feedback design for the Buck Converter Portland State University Department of Electrical and Computer Engineering Portland, Oregon, USA December 30, 2009 Abstract In this paper we explore two compensation topologies for the Buck DC to DC power converter, dominant pole and dominant pole with zero compensation. These feedback systems are developed and implemented with an Op-Amp circuit design, and each system is tested with a step disturbance at the system input voltage. Each system response is compared to the uncompensated converter through simulation and Bode plot analysis. Introduction The Buck converter, shown in Figure 1, is a simple converter topology that has several applications in DC to DC power conversion. The aim of this report is to explore the behavior of this converter in response to step disturbances to the system input, and explore a few compensation techniques to improve the converter s response to those input disturbances. Particularly, different varieties of dominant pole compensation will be explored involving two implementations of Proportional Integral (PI) compensation. Figure 1: The ideal Buck converter (Source: Erickson) Section one will explore the uncompensated Buck converter, and how the system responds to a voltage step at the input. Section two will describe a dominant pole compensation technique, which will act to decrease the effect of the step response at the output. In section three, a zero will be added to the system at the corner frequency of the Buck converter and section four will reduce the peaking of the system. Each technique has it s advantages, and each will be explored. 1) The Uncompensated Buck Converter Figure 1 shows the topology of the Buck converter. Using Steady-State analysis techniques, the output of the converter can be calculated to be equal to DV g, the duty cycle of the switch multiplied by the input 1

voltage. Typically, a Pulse Width Modulated (PWM) signal is used to drive the switch in the circuit. Figure 2 [1] shows a basic buck converter PWM control loop. For the purpose of this analysis, the circuit is designed to operate in continuous conduction mode, with the input to the system as a step response from 28V 30V 28V. Figure 2: Buck converter control loop (Source: Erickson) The basic topology for the converter control loop is shown above, where G c is the compensation scheme used in the circuit, V m is the transfer function of the pulse width modulator, and H(s) is the conversion factor. The conversion factor is used to reduce the amplitude of the output to a level that will cancel the value of the system reference voltage. In practice, there will always be a small difference between H(s)V (s) and the reference, which is defined as the error signal V e. With a large enough compensation loop gain, the error signal will be able to provide enough voltage for the output to follow the reference [1, p. 332]. For the purpose of this report, assume that G vg applies step disturbances to the system and Z out has no contribution to the system response. From [1], the transfer function of a Buck converter can be shown to be equal to the function below, where G p (s) = G p (s) = G p0 1 + s Qω 0 + ( ) 2, (1) s ω 0 G p0 1 + sl R + s2 LC, (2) For the converter topology of this paper, the parameter values of the transfer function are shown below: G p0 = V g = 28, f 0 = ω 0 2π = 1 2π LC C = 1KHz, and Q = R L = 9.49 = 19.5dB 2

The loop gain of the system is defined as T (s) = G c (s)g p (s)h(s)g pwm (s) = T 0 1 + s Qω 0 + ( ) 2 s ω 0 Using the given values for the control loop, and setting G c (s) = 1 for an uncompensated converter, the values of the control loop variables can be defined as shown below: T 0 = G c (s)h(s)g pwm (s) = 2.33, G c = 1, H(s) = 1 3, and G pwm = 1 4 An asymptotic Bode plot has been created for the system and is shown in Figure 3. For this uncompensated converter design, the phase margin is read to be 0. Realistically, the phase margin is a small positive value since the phase never reaches 180, but is on the verge of instability. This could be a problem if the feedback loop was closed on this system, but for this portion the system is in an open loop configuration. Since the phase only approaches 180 but never reaches it, the gain margin is defined as infinite. Figure 3: Uncompensated Buck converter Figure 4 shows the response of the uncompensated Buck to a step disturbance at it s input. Because the system is uncompensated, the step response is translated to the the output of the system. In the following sections, compensation techniques will be explored to improve the system reponse to changes in the input voltage. 2) Dominant Pole Compensation (3 db gain margin) One way to improve the response of the buck converter is to introduce dominant pole compensation. Dominant pole compensation introduces an integrating circuit into a feedback loop. This particular integrating 3

Figure 4: Uncompensated Buck converter system response to input voltage step circuit will serve two purposes. The first will be to increase the phase margin so the system will be stable in a feedback configuration. The second is to design the converter with less gain to improve the system stability. Figure 5 is an Op-Amp implementation of an integrator, or dominant pole compensation. The basic equation for a dominant pole is shown below, and is incorporated into the loop gain of the system. Figure 5: Dominant pole op-amp implementation G c (s) = G c0 s (3) T 0 G c0 T (s) = ( ( ) ) 2 (4) s 1 + s s Qω 0 + ω 0 To design this system for a 3 db gain margin, it is required for the gain to be equal to.707 where the phase crosses 180. Using Bode plot analysis (see Figure 7), the frequency where the phase is equal to 4

180 is found to be 1000 Hz. Using previously calculated parameters and the given values, the gain of the compensator can be calculated, as shown below. T 0 G c0 Q 2πf 0 = 3 db =.707 G c0 = G c0 = 2πf 0(.707) T 0 Q 2π (1000 Hz) (.707) (2.33)(9.49) G c0 = 201 In the equation below, resistor and capacitor component values are calculated to realize the gain of the system. Setting R1 = 10kΩ, C1 = G c (s) = G c0 s = 1 s 1 R 1 C 1 (5) G c0 = 1 R 1 C 1 (6) 1 G c0 R1 = 1 (201)(10kΩ) = 0.5μF Figure 6: Compensation transfer function 5

Figure 7: Dominant pole compensation loop gain From the asymptotic bode plot (Figure 7), the gain and the phase margin of the system can be calculated directly. By design, the gain margin is equal to 3 db. fc = (2.33)(201) = 74 Hz 2π φ M = 180 90 = 90 T 0 G c0 Q 2πf 0 = 3 db =.707 G M = 3 db Figure 8 shows the response of the dominant pole compensation to a step disturbance at its input. Because of the high Q factor in the system, there is definite overshoot and oscillation in the response as the output decays back down to the expected value of 15 Volts. Clearly, the dominant pole compensation is working to oppose the step disturbance on the input. Next we will explore the effect of adding a zero at the system corner frequency. 3) Dominant Pole with Zero Compensation ( 3 db gain margin) To obtain better performance and control of this system it can be advantageous to incorporate a zero, at some higher frequency, to the transfer function. Specifically, a zero will be placed at the corner frequency of the Buck converter. A zero will act to reduce the effect of the second order complex pole, which will decrease the roll off. The phase at 1000 Hz will be effected by the zero, and rise from 180 to 135. As a 6

Figure 8: Step response of dominant pole compensated buck converter starting point for the design, the feedback system uses this frequency for the gain margin, even though the gain margin will change. The transfer function of the compensator is shown below, as well as the changes to the complete transfer function. ) G c0 (1 + s ω z G c (s) = (7) s 1 + s ω T (s) = T 0 G z c0 ( ( ) ) 2 (8) s 1 + s s Qω 0 + ω 0 Analysis of this compensator topology is very similar to that of the dominant pole compensator. With the zero occuring at the corner frequency of the system, G c0 will be the same value. To achieve the form of the transfer function shown in Equation 7, a PI Op-Amp topology will be used. Calculating the transfer function of the Op-Amp circuit shown in Figure 10, and substituting the parameters of the system, components values are calculated to realize the compensation scheme. V out = 1 (scr 2 + 1) = 1 s 1 + 1 CR 2 V in R 1 C s R 1 C s It can be seen from the equation above that ω z = 1 CR 2 and G c0 = 1 CR 1. Using the calculated gain value (G c0 = 201), setting R 2 = 10kΩ and realizing that f 0 = 1kHz, the unknown component values can be calculated. C = 1 1 = R 2 ω 0 2π(1kHz)(10kΩ) = 15nF R 1 = 1 1 = CG c0 201(15nF ) = 311kΩ Figure 12 shows the response of the dominant pole with zero compensation to a step disturbance at it s input. Similar to the dominant pole compensation, the system provides PI compensation and the step disturbances are corrected. Although this system s stability has been improved, the output is observed to be nearly the same. 7

Figure 9: Dominant pole with zero compensation Figure 10: Dominant pole with zero Op-Amp implementation The phase margin for this system is identical to that of the previous compensation design, because the added zero occurs after the unity-gain crossover point. To calculate the gain margin it s necessary to know where the phase crosses 180. To determine this value, the phase at the lowest point presented on the asymptotic bode plot in Figure 11 needs to be calculated. The exact formula for the phase can be found on 8

Figure 11: Dominant pole with zero compensation loop gain Figure 12: Step response of dominant pole with zero compensated buck converter ( 3 db gain margin) the bode plot and is also shown below: 1 f Q f 0 90 + atan( f ) atan( f 0 1 ( f f 0 ) ) = φ 2 9

Taking the frequencies shown on the bode plot and using the formula shown above, the exact phase at its lowest point is: 90 + atan( 1.136kHz 1.13 9.49 ) atan( 1kHz 1 (1.13) 2 ) = 145.35 According to the above calculation, the approximations made using bode plot analysis shows that there is a significant deviation from the value of the actual phase. The phase of the converter never crosses 180 even at it s lowest point. Therefore, the gain margin is by definition infinite. In the final section, this feedback topology will be adjusted so the peaking of the system at the corner frequency is lowered from -3dB to approximately -10 db. 4) Dominant Pole with Zero Compensation (>10 db gain margin) For this design, the topology from section three will be modified to reduce the peaking to -10 db (or.32) below unity. The PI compensator will functionally remain the same, only the value of G c0 will change to account for the lower peaking. Using the equation for G c0 shown in Figure 11 G c0 = 2πf 0(.32) T 0 Q = 2π(1000Hz)(.32) 2.33(9.49) G c0 = 45.4 Figure 13: Step response of dominant pole with zero compensated Buck converter (>10 db gain margin) Using the PI compensator shown in section 3 and assuming that R 2 = 10kΩ, solving for the new value of R 1 : R 1 = 1 1 = R 2 G c0 45.4(15nF ) = 1.3MΩ The value of the capacitor will not change. For gain and phase margins, f c = G c0t 0 2π = 45.4(2.33) 2π = 16.8Hz 10

Because only the gain of the system was reduced in this design, the bode plot is essentially the same, only with the gain of the system shifted down. The phase and gain margin are identical to that of section three. Figure 13 shows the response of the dominant pole with zero compensation to a step disturbance at it s input. With the inclusion of lower peaking, it is evident that the the system responds much slower to a step disturbance at the input. The system has less bandwidth and is slower to respond to disturbances. Conclusion The uncompensated Buck converter and three compensation methods were analyzed. The compensation methods have feedback which improve the stability of the output voltage in response to input disturbances. The uncompensated Buck converter simulations showed that input step disturbances directly affected the output of the system. The output never stabilized at the value it was designed for with the disturbance. Through interpretation of the output, it is realized that the uncompensated Buck converter implementation is unstable. The first compensated design used a dominant pole. The simulation results showed the feedback of the system compensated for the input step disturbance and the output stabilized at the designed value. The next compensated design used a dominant pole with a zero added at the corner frequency. The simulation results were very similar to the first compensated design, even though the stability was increased. The last compensated design was the same as the previous, but with the system peaking lowered from -3dB to -10dB. The simulation results showed slower response to an input step disturbance; a result of the stability being increased. The increase in stability also decreased the bandwidth. For this application the second compensated design had the best results. The stability was increased over that of the first design while the response time was comparable, and the fastest of all options considered. For applications where stability is a priority concern, it may be desirable to choose the last compensated design. The response time of the system will be compromised, but for greater stability. References [1] Robert W. Erickson and Dragan Maksimović. Fundamentals of Power Electronics. Springer Science+Business Media, LLC, second edition, 2001. 11

12 Figure 14: PECS schematic of uncompensated Buck converter

13 Figure 15: PECS schematic of dominant pole compensated Buck converter

14 Figure 16: PECS schematic of dominant pole with zero compensated Buck converter ( 3dB)

15 Figure 17: PECS schematic of dominant pole with zero compensated Buck converter (>10dB)