Prototype 2nd order system:

Slides:



Advertisements
Similar presentations
Lect. 5 Lead-Lag Control Basil Hamed
Advertisements

University of Virginia Proportional Control Spring 2015 Jack Stankovic University of Virginia.
سیستمهای کنترل خطی پاییز 1389 بسم ا... الرحمن الرحيم دکتر حسين بلندي - دکتر سید مجید اسما عیل زاده.
MESB374 System Modeling and Analysis PID Controller Design
Time domain response specifications Defined based on unit step response with i.c. = 0 Defined for closed-loop system.
Lec 6. Second Order Systems
Section 11.1 Section 11.2 Conic Sections The Parabola.
Lec 7. Higher Order Systems, Stability, and Routh Stability Criteria Higher order systems Stability Routh Stability Criterion Reading: 5-4; 5-5, 5.6 (skip.
1 Time Response. CHAPTER Poles and Zeros and System Response. Figure 3.1: (a) System showing input and output; (b) Pole-zero plot of the system;
The Coordinate Plane 101 ALGEBRA 11/16/15. The coordinate plane is a set of axis on which ordered pairs of input and output values can be plotted.
Dynamic Response Steady State Response: the part of response when t → ∞ Transient response: the part of response right after the input is being applied.
Margins on Bode plot. Margins on Nyquist plot Suppose: Draw Nyquist plot G(jω) & unit circle They intersect at point A Nyquist plot cross neg. real axis.
Time domain response specifications
SKEE 3143 Control Systems Design Chapter 2 – PID Controllers Design
System Dynamics Dr. Mohammad Kilani
Lecture 7/8 Analysis in the time domain (II) North China Electric Power University Sun Hairong.
Part B – Effect of Feedback on BW
Automatic Control Theory CSE 322
Lesson 20: Process Characteristics- 2nd Order Lag Process
Youngjune, Han Chapter 4 Time Response Youngjune, Han
Control Response Patterns
Time Response Analysis
Transient Response First order system transient response
Effects of Zeros and Additional Poles
Lec 9. Root Locus Analysis I
Control System Analysis and Design by the Frequency Response Method
Introduction to the coordinate Plane
Part B – Effect of Feedback on BW
Frequency Domain Design Demo I EE 362K (Buckman) Fall 03
Controller design by R.L.
UNIT-III STABILITY ANALYSIS.
Instructor: Jongeun Choi
Chapter 2 Functions.
Transient Response First order system transient response
What damping ratio range do we typically want?___0.4~1____
Name:_________________
Eigenvalues: p1=-4.526, p2,3= ±2.7883i, p4=
Algebra Review.
Controller design by R.L.
Prototype 2nd order system:
System type, steady state tracking, & Bode plot
Time Response System & Control Engineering Lab.
Graphing on the Coordinate Plane
Feedback: Principles & Analysis
Root Loci Analysis (3): Root Locus Approach to Control System Design
Stability from Nyquist plot
UNIT-II TIME RESPONSE ANALYSIS
UNIVERSITI MALAYSIA PERLIS SCHOOL OF ELECTRICAL SYSTEM ENGINEERING
Margins on Bode plots G(s) + -.
Graphing Linear Equations
With respect to reference input:
The root locus technique
Response of Higher Order Systems
EIE 211 : Electronic Devices and Circuit Design II
7-5 Relative Stability.
Root-Locus Analysis (2)
Chapter 4. Time Response I may not have gone where I intended to go, but I think I have ended up where I needed to be. Pusan National University Intelligent.
Graphing on the Coordinate Plane
Control System Toolbox (Part-II)
CH. 3 Time Response Chapter3. Time Response.
CH. 6 Root Locus Chapter6. Root Locus.
Eigenvalues: p1=-4.526, p2,3= ±2.7883i, p4=
2a. Transfer function of closed loop system
Graphing Linear Equations
IntroductionLecture 1: Basic Ideas & Terminology
Lecture 24 Time-Domain Response for IIR Systems
Chapter 5 – The Performance of Feedback Control Systems
Time Response, Stability, and
By: Nafees Ahamad, AP, EECE, Dept. DIT University, Dehradun
Presentation transcript:

Prototype 2nd order system: target

Type 1: Settling time: = (3 or 4 or 5)/s For 5%, 2%, 1% tol

Pole location determines transient

All closed-loop poles must be strictly in the left half planes Transient dies away Dominant poles: those which contribute the most to the transient Typically have dominant pole pair (complex conjugate) Closest to jω-axis (i.e. the least negative) Slowest to die away

Typical design specifications Steady-state: ess to step ≤ # % ts ≤ · · · Speed (responsiveness) tr ≤ · · · td ≤ · · · Relative stability Mp ≤ · · · %

These specs translate into requirements on ζ, ωn or on closed-loop pole location : Find ranges for ζ and ωn so that all 3 are satisfied.

Find conditions on σ and ωd.

In the complex plane : Any pole on the ray have the same z p=-s + jwd Mp < … or z > … corresponds to a conic region about the neg real axis j -s

Constant σ : vertical lines σ > # is half plane Any poles on the same vertical line have the same s, and the same settling time ts s=1 or ts=5 s>2 or ts=2.5 ts < … corresponds to a half plane to the left of a vertical line

Constant ωd : horizontal line ωd < · · · is a band ωd > · · · is the plane excluding band Any poles on the same horizontal line have the same wd, and the same oscillation frequency A centered horizontal band corresponds to oscillation frequency < … The plane excluding a centered horizontal band corresponds to oscillation frequency > …

ωn < · · · inside of a circle ωn > · · · outside of a circle Constant ωn : circles ωn < · · · inside of a circle ωn > · · · outside of a circle Any poles on the same circle have the same wn, and similar rise time/delay time Inside circle corresponds to tr> … Outside a circle corresponds to tr < …

Constant ζ : φ = cos-1ζ constant Constant ζ = ray from the origin ζ > · · · is the cone ζ < · · · is the other part

If more than one requirement, get the common (overlapped) area e.g. ζ > 0.5, σ > 2, ωn > 3 gives Sometimes meeting two will also meet the third, but not always.

Try to remember these:

When given unit step input, the output looks like: Example: + - When given unit step input, the output looks like: Q: estimate k and τ.

When given unit step input, the output looks like: Example: + - When given unit step input, the output looks like: Q: estimate k and τ. Yss = ____; is it prototype? Mp = ____; tp = ____; 5% ts = ____

Solve for J and t

Effects of additional zeros Suppose we originally have: i.e. step response Now introduce a zero at s = -z The new step response:

Effects: Increased speed, Larger overshoot, Might increase ts

When z < 0, the zero s = -z is > 0, is in the right half plane. Such a zero is called a nonminimum phase zero. A system with nonminimum phase zeros is called a nonminimum phase system. Nonminimum phase zero should be avoided in design. i.e. Do not introduce such a zero in your controller.

Effects of additional pole Suppose, instead of a zero, we introduce a pole at s = -p, i.e.

L.P.F. has smoothing effect, or averaging effect Effects: Slower, Reduced overshoot, May increase or decrease ts