MT-033: Voltage Feedback Op Amp Gain and Bandwidth
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Lesson 22: Determining Control Stability Using Bode Plots
11/30/2015 Lesson 22: Determining Control Stability Using Bode Plots 1 ET 438A AUTOMATIC CONTROL SYSTEMS TECHNOLOGY lesson22et438a.pptx Learning Objectives 2 After this presentation you will be able to: List the control stability criteria for open loop frequency response. Identify the gain and phase margins necessary for a stable control system. Use a Bode plot to determine if a control system is stable or unstable. Generate Bode plots of control systems the include dead-time delay and determine system stability. lesson22et438a.pptx 1 11/30/2015 Bode Plot Stability Criteria 3 Open loop gain of less than 1 (G<1 or G<0dB) at Stable Control open loop phase angle of -180 degrees System Oscillatory Open loop gain of exactly 1 (G=1 or G= 0dB) at Control System open loop phase angle of -180 degrees Marginally Stable Unstable Control Open loop gain of greater than 1 (G>1 or G>0dB) System at open loop phase angle of -180 degrees lesson22et438a.pptx Phase and Gain Margins 4 Inherent error and inaccuracies require ranges of phase shift and gain to insure stability. Gain Margin – Safe level below 1 required for stability Minimum level : G=0.5 or -6 dB at phase shift of 180 degrees Phase Margin – Safe level above -180 degrees required for stability Minimum level : f=40 degree or -180+ 40=-140 degrees at gain level of 0.5 or 0 dB. lesson22et438a.pptx 2 11/30/2015 Determining Phase and Gain Margins 5 Define two frequencies: wodB = frequency of 0 dB gain w180 = frequency of -180 degree phase shift Open Loop Gain 0 dB Gain Margin -m180 bodB Phase Margin -180+b0dB -180o Open Loop w w Phase odB 180 lesson22et438a.pptx Determining Phase and Gain Margins 6 Procedure: 1) Draw vertical lines through 0 dB on gain and -180 on phase plots. -
Op Amp Stability and Input Capacitance
Amplifiers: Op Amps Texas Instruments Incorporated Op amp stability and input capacitance By Ron Mancini (Email: [email protected]) Staff Scientist, Advanced Analog Products Introduction Figure 1. Equation 1 can be written from the op Op amp instability is compensated out with the addition of amp schematic by opening the feedback loop an external RC network to the circuit. There are thousands and calculating gain of different op amps, but all of them fall into two categories: uncompensated and internally compensated. Uncompen- sated op amps always require external compensation ZG ZF components to achieve stability; while internally compen- VIN1 sated op amps are stable, under limited conditions, with no additional external components. – ZG VOUT Internally compensated op amps can be made unstable VIN2 + in several ways: by driving capacitive loads, by adding capacitance to the inverting input lead, and by adding in ZF phase feedback with external components. Adding in phase feedback is a popular method of making an oscillator that is beyond the scope of this article. Input capacitance is hard to avoid because the op amp leads have stray capaci- tance and the printed circuit board contributes some stray Figure 2. Open-loop-gain/phase curves are capacitance, so many internally compensated op amp critical stability-analysis tools circuits require external compensation to restore stability. Output capacitance comes in the form of some kind of load—a cable, converter-input capacitance, or filter 80 240 VDD = 1.8 V & 2.7 V (dB) 70 210 capacitance—and reduces stability in buffer configurations. RL= 2 kΩ VD 60 180 CL = 10 pF 150 Stability theory review 50 TA = 25˚C 40 120 Phase The theory for the op amp circuit shown in Figure 1 is 90 β 30 taken from Reference 1, Chapter 6. -
EE C128 Chapter 10
Lecture abstract EE C128 / ME C134 – Feedback Control Systems Topics covered in this presentation Lecture – Chapter 10 – Frequency Response Techniques I Advantages of FR techniques over RL I Define FR Alexandre Bayen I Define Bode & Nyquist plots I Relation between poles & zeros to Bode plots (slope, etc.) Department of Electrical Engineering & Computer Science st nd University of California Berkeley I Features of 1 -&2 -order system Bode plots I Define Nyquist criterion I Method of dealing with OL poles & zeros on imaginary axis I Simple method of dealing with OL stable & unstable systems I Determining gain & phase margins from Bode & Nyquist plots I Define static error constants September 10, 2013 I Determining static error constants from Bode & Nyquist plots I Determining TF from experimental FR data Bayen (EECS, UCB) Feedback Control Systems September 10, 2013 1 / 64 Bayen (EECS, UCB) Feedback Control Systems September 10, 2013 2 / 64 10 FR techniques 10.1 Intro Chapter outline 1 10 Frequency response techniques 1 10 Frequency response techniques 10.1 Introduction 10.1 Introduction 10.2 Asymptotic approximations: Bode plots 10.2 Asymptotic approximations: Bode plots 10.3 Introduction to Nyquist criterion 10.3 Introduction to Nyquist criterion 10.4 Sketching the Nyquist diagram 10.4 Sketching the Nyquist diagram 10.5 Stability via the Nyquist diagram 10.5 Stability via the Nyquist diagram 10.6 Gain margin and phase margin via the Nyquist diagram 10.6 Gain margin and phase margin via the Nyquist diagram 10.7 Stability, gain margin, and -
I Introduction and Background
Final Design Report Platform Motion Measurement System ELEC 492 A Senior Design Project, 2005 Between University of San Diego And Trex Enterprises Submitted to: Dr. Lord at USD Prepared by: YAZ Zlatko Filipovic Yoshitaka Yano August 12, 2005 University of San Diego Final Design Report USD August 12, 2005 Platform Motion Measurement System Table of Contents I. Acknowledgments…………...…………………………………………………………4 II. Executive Summary……..…………………………………………………………….5 III. Introduction and Background…...………………………...………………………….6 IV. Project Requirements…………….................................................................................8 V. Methodology of Design Plan……….…..……………..…….………….…..…….…..11 VI. Testing….……………………………………..…..…………………….……...........21 VII. Deliverables and Project Results………...…………...…………..…….…………...24 VIII. Budget………………………………………...……..……………………………..25 IX. Personnel…………………..………………………………………....….……….......28 X. Design Schedule………….…...……………………………….……...…………........29 XI. Reference and Bibliography…………..…………..…………………...…………….31 XII. Summary…………………………………………………………………………....32 Appendices Appendix 1. Simulink Simulations…..………………………….…….33 Appendix 2. VisSim Simulations..........……………………………….34 Appendix 3. Frequency Response and VisSim results……………......36 Appendix 4. Vibration Measurements…………..………………….….38 Appendix 5. PCB Layout and Schematic……………………………..39 Appendix 6. User’s Manual…………………………………………..41 Appendix 7. PSpice Simulations of Hfilter…………………………….46 1 Final Design Report USD August 12, 2005 Platform Motion Measurement System -
Meeting Design Specifications
NDSU Meeting Design Specs using Bode Plots ECE 461 Meeting Design Specs using Bode Plots When designing a compensator to meet design specs including: Steady-state error for a step input Phase Margin 0dB gain frequency the procedure using Bode plots is about the same as it was for root-locus plots. Add a pole at s = 0 if needed (making the system type-1) Start cancelling zeros until the system is too fast For every zero you added, add a pole. Place these poles so that the phase adds up. When using root-locus techniques, the phase adds up to 180 degrees at some spot on the s-plane. When using Bode plot techniques, the phase adds up to give you your phase margin at some spot on the jw axis. Example 1: Problem: Given the following system 1000 G(s) = (s+1)(s+3)(s+6)(s+10) Design a compensator which result in No error for a step input 20% overshoot for a step input, and A settling time of 4 second Solution: First, convert to Bode Plot terminology No overshoot means make this a type-1 system. Add a pole at s = 0. 20% overshoot means ζ = 0.4559 Mm = 1.2322 GK = 1∠ − 132.120 Phase Margin = 47.88 degrees A settling time of 4 seconds means s = -1 + j X s = -1 + j2 (from the damping ratio) The 0dB gain frequency is 2.00 rad/sec In short, design K(s) so that the system is type-1 and 0 (GK)s=j2 = 1∠ − 132.12 JSG 1 rev June 22, 2016 NDSU Meeting Design Specs using Bode Plots ECE 461 Start with s+1 K(s) = s At 4 rad/sec 1000 0 GK = s(s+3)(s+6)(s+10) = 2.1508∠ − 153.43 s=j2 There is too much phase shift, so start cancelling zeros. -
Applications Academic Program Distributing Vissim Models
VISSIM VisSim is a visual block diagram language for simulation of dynamical systems and Model Based Design of embedded systems. It is developed by Visual Solutions of Westford, Massachusetts. Applications VisSim is widely used in control system design and digital signal processing for multidomain simulation and design. It includes blocks for arithmetic, Boolean, and transcendental functions, as well as digital filters, transfer functions, numerical integration and interactive plotting. The most commonly modeled systems are aeronautical, biological/medical, digital power, electric motor, electrical, hydraulic, mechanical, process, thermal/HVAC and econometric. Academic program The VisSim Free Academic Program allows accredited educational institutions to site license VisSim v3.0 for no cost. The latest versions of VisSim and addons are also available to students and academic institutions at greatly reduced pricing. Distributing VisSim models VisSim viewer screenshot with sample model. The free Vis Sim Viewer is a convenient way to share VisSim models with colleagues and clients not licensed to use VisSim. The VisSim Viewer will execute any VisSim model, and allows changes to block and simulation parameters to illustrate different design scenarios. Sliders and buttons may be activated if included in the model. Code generation The VisSim/C-Code add-on generates efficient, readable ANSI C code for algorithm acceleration and real-time implementation of embedded systems. The code is more efficient and readable than most other code generators. VisSim's author served on the X3J11 ANSI C committee and wrote several C compilers, in addition to co-authoring a book on C. [2] This deep understanding of ANSI C, and the nature of the resulting machine code when compiled, is the key to the code generator's efficiency. -
OA-25 Stability Analysis of Current Feedback Amplifiers
OBSOLETE Application Report SNOA371C–May 1995–Revised April 2013 OA-25 Stability Analysis of Current Feedback Amplifiers ..................................................................................................................................................... ABSTRACT High frequency current-feedback amplifiers (CFA) are finding a wide acceptance in more complicated applications from dc to high bandwidths. Often the applications involve amplifying signals in simple resistive networks for which the device-specific data sheets provide adequate information to complete the task. Too often the CFA application involves amplifying signals that have a complex load or parasitic components at the external nodes that creates stability problems. Contents 1 Introduction .................................................................................................................. 2 2 Stability Review ............................................................................................................. 2 3 Review of Bode Analysis ................................................................................................... 2 4 A Better Model .............................................................................................................. 3 5 Mathematical Justification .................................................................................................. 3 6 Open Loop Transimpedance Plot ......................................................................................... 4 7 Including Z(s) ............................................................................................................... -
Frequency Response and Bode Plots
1 Frequency Response and Bode Plots 1.1 Preliminaries The steady-state sinusoidal frequency-response of a circuit is described by the phasor transfer function Hj( ) . A Bode plot is a graph of the magnitude (in dB) or phase of the transfer function versus frequency. Of course we can easily program the transfer function into a computer to make such plots, and for very complicated transfer functions this may be our only recourse. But in many cases the key features of the plot can be quickly sketched by hand using some simple rules that identify the impact of the poles and zeroes in shaping the frequency response. The advantage of this approach is the insight it provides on how the circuit elements influence the frequency response. This is especially important in the design of frequency-selective circuits. We will first consider how to generate Bode plots for simple poles, and then discuss how to handle the general second-order response. Before doing this, however, it may be helpful to review some properties of transfer functions, the decibel scale, and properties of the log function. Poles, Zeroes, and Stability The s-domain transfer function is always a rational polynomial function of the form Ns() smm as12 a s m asa Hs() K K mm12 10 (1.1) nn12 n Ds() s bsnn12 b s bsb 10 As we have seen already, the polynomials in the numerator and denominator are factored to find the poles and zeroes; these are the values of s that make the numerator or denominator zero. If we write the zeroes as zz123,, zetc., and similarly write the poles as pp123,, p , then Hs( ) can be written in factored form as ()()()s zsz sz Hs() K 12 m (1.2) ()()()s psp12 sp n 1 © Bob York 2009 2 Frequency Response and Bode Plots The pole and zero locations can be real or complex. -
Chapter 6 Amplifiers with Feedback
ELECTRONICS-1. ZOLTAI CHAPTER 6 AMPLIFIERS WITH FEEDBACK Purpose of feedback: changing the parameters of the amplifier according to needs. Principle of feedback: (S is the symbol for Signal: in the reality either voltage or current.) So = AS1 S1 = Si - Sf = Si - ßSo Si S1 So = A(Si - S ) So ß o + A from where: - Sf=ßSo * So A A ß A = Si 1 A 1 H where: H = Aß Denominations: loop-gain H = Aß open-loop gain A = So/S1 * closed-loop gain A = So/Si Qualitatively different cases of feedback: oscillation with const. amplitude oscillation with narrower growing amplitude pos. f.b. H -1 0 positive feedback negative feedback Why do we use almost always negative feedback? * The total change of the A as a function of A and ß: 1(1 A) A A 2 A* = A (1 A) 2 (1 A) 2 Introducing the relative errors: A * 1 A A A * 1 A A 1 A According to this, the relative error of the open loop gain will be decreased by (1+Aß), and the error of the feedback circuit goes 1:1 into the relative error of the closed loop gain. This is the Elec1-fb.doc 52 ELECTRONICS-1. ZOLTAI reason for using almost always the negative feedback. (We can not take advantage of the negative sign, because the sign of the relative errors is random.) Speaking of negative or positive feedback is only justified if A and ß are real quantities. Generally they are complex quantities, and the type of the feedback is a function of the frequency: E.g. -
Operational Amplifiers: Part 3 Non-Ideal Behavior of Feedback
Operational Amplifiers: Part 3 Non-ideal Behavior of Feedback Amplifiers AC Errors and Stability by Tim J. Sobering Analog Design Engineer & Op Amp Addict Copyright 2014 Tim J. Sobering Finite Open-Loop Gain and Small-signal analysis Define VA as the voltage between the Op Amp input terminals Use KCL 0 V_OUT = Av x Va + + Va OUT V_OUT - Note the - Av “Loop Gain” – Avβ β V_IN Rg Rf Copyright 2014 Tim J. Sobering Liberally apply algebra… 0 0 1 1 1 1 1 1 1 1 Copyright 2014 Tim J. Sobering Get lost in the algebra… 1 1 1 1 1 1 1 Copyright 2014 Tim J. Sobering More algebra… Recall β is the Feedback Factor and define α 1 1 1 1 1 Copyright 2014 Tim J. Sobering You can apply the exact same analysis to the Non-inverting amplifier Lots of steps and algebra and hand waving yields… 1 This is very similar to the Inverting amplifier configuration 1 Note that if Av → ∞, converges to 1/β and –α /β –Rf /Rg If we can apply a little more algebra we can make this converge on a single, more informative, solution Copyright 2014 Tim J. Sobering You can apply the exact same analysis to the Non-inverting amplifier Non-inverting configuration Inverting Configuration 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 Copyright 2014 Tim J. Sobering Inverting and Non-Inverting Amplifiers “seem” to act the same way Magically, we again obtain the ideal gain times an error term If Av → ∞ we obtain the ideal gain 1 1 1 Avβ is called the Loop Gain and determines stability If Avβ –1 1180° the error term goes to infinity and you have an oscillator – this is the “Nyquist Criterion” for oscillation Gain error is obtained from the loop gain 1 For < 1% gain error, 40 dB 1 (2 decades in bandwidth!) 1 Copyright 2014 Tim J. -
A Note on Stability Analysis Using Bode Plots
ChE classroom A NOTE ON STABILITY ANALYSIS USING BODE PLOTS JUERGEN HAHN, THOMAS EDISON, THOMAS F. E DGAR The University of Texas at Austin • Austin, TX 78712-1062 he Bode plot is an important tool for stability analysis amplitude ratio greater than unity for frequencies where f = of closed-loop systems. It is based on calculating the -180∞-n*360∞, where n is an integer. These conditions can T amplitude and phase angle for the transfer function occur when the process includes time delays, as shown in the following example. GsGsGs 1 OL( ) = C( ) P ( ) ( ) for s = jw Juergen Hahn was born in Grevenbroich, Ger- many, in 1971. He received his diploma degree where GC(s) is the controller and GP(s) is the process. The in engineering from RWTH Aachen, Germany, Bode stability criterion presented in most process control text- in 1997, and his MS degree in chemical engi- neering from the University of Texas, Austin, in books is a sufficient, but not necessary, condition for insta- 1998. He is currently a PhD candidate working bility of a closed-loop process.[1-4] Therefore, it is not pos- as a research assistant in chemical engineer- sible to use this criterion to make definitive statements about ing at the University of Texas, Austin. His re- search interests include process modeling, non- the stability of a given process. linear model reduction, and nonlinearity quanti- fication. Other textbooks[5,6] state that this sufficient condition is a necessary condition as well. That statement is not correct, as Thomas Edison is a lecturer at the University of Texas, Austin. -
How to Measure the Loop Transfer Function of Power Supplies (Rev. A)
Application Report SNVA364A–October 2008–Revised April 2013 AN-1889 How to Measure the Loop Transfer Function of Power Supplies ..................................................................................................................................................... ABSTRACT This application report shows how to measure the critical points of a bode plot with only an audio generator (or simple signal generator) and an oscilloscope. The method is explained in an easy to follow step-by-step manner so that a power supply designer can start performing these measurements in a short amount of time. Contents 1 Introduction .................................................................................................................. 2 2 Step 1: Setting up the Circuit .............................................................................................. 2 3 Step 2: The Injection Transformer ........................................................................................ 4 4 Step 3: Preparing the Signal Generator .................................................................................. 4 5 Step 4: Hooking up the Oscilloscope ..................................................................................... 4 6 Step 5: Preparing the Power Supply ..................................................................................... 4 7 Step 6: Taking the Measurement ......................................................................................... 5 8 Step 7: Analyzing a Bode Plot ...........................................................................................