Control System Engineering (EE301T) Assignment: 2

Similar documents
Lecture 1: Growth and decay of current in RL circuit. Growth of current in LR Circuit. D.K.Pandey

whereby we can express the phase by any one of the formulas cos ( 3 whereby we can express the phase by any one of the formulas

Lecture 2: Current in RC circuit D.K.Pandey

CSE 245: Computer Aided Circuit Simulation and Verification

Charging of capacitor through inductor and resistor

UNIT #5 EXPONENTIAL AND LOGARITHMIC FUNCTIONS

a dt a dt a dt dt If 1, then the poles in the transfer function are complex conjugates. Let s look at f t H t f s / s. So, for a 2 nd order system:

Boyce/DiPrima 9 th ed, Ch 2.1: Linear Equations; Method of Integrating Factors

MEM 355 Performance Enhancement of Dynamical Systems A First Control Problem - Cruise Control

C From Faraday's Law, the induced voltage is, C The effect of electromagnetic induction in the coil itself is called selfinduction.

AR(1) Process. The first-order autoregressive process, AR(1) is. where e t is WN(0, σ 2 )

H is equal to the surface current J S

EXERCISE - 01 CHECK YOUR GRASP

Phys463.nb Conductivity. Another equivalent definition of the Fermi velocity is

General Article Application of differential equation in L-R and C-R circuit analysis by classical method. Abstract

Microscopic Flow Characteristics Time Headway - Distribution

REPETITION before the exam PART 2, Transform Methods. Laplace transforms: τ dτ. L1. Derive the formulas : L2. Find the Laplace transform F(s) if.

Spring 2006 Process Dynamics, Operations, and Control Lesson 2: Mathematics Review

Lecture 1: Numerical Integration The Trapezoidal and Simpson s Rule

Inverse Fourier Transform. Properties of Continuous time Fourier Transform. Review. Linearity. Reading Assignment Oppenheim Sec pp.289.

Copyright 2012 Pearson Education, Inc. Publishing as Prentice Hall.

Applied Statistics and Probability for Engineers, 6 th edition October 17, 2016

5. An object moving along an x-coordinate axis with its scale measured in meters has a velocity of 6t

2. NONLINEAR DYNAMICS MODEL FOR A

Review Lecture 5. The source-free R-C/R-L circuit Step response of an RC/RL circuit. The time constant = RC The final capacitor voltage v( )

S.Y. B.Sc. (IT) : Sem. III. Applied Mathematics. Q.1 Attempt the following (any THREE) [15]

1. Inverse Matrix 4[(3 7) (02)] 1[(0 7) (3 2)] Recall that the inverse of A is equal to:

Physics 160 Lecture 3. R. Johnson April 6, 2015

Chapter 3: Fourier Representation of Signals and LTI Systems. Chih-Wei Liu

4.1 The Uniform Distribution Def n: A c.r.v. X has a continuous uniform distribution on [a, b] when its pdf is = 1 a x b

CHAPTER 9 Compressible Flow

2.1. Differential Equations and Solutions #3, 4, 17, 20, 24, 35

Let s look again at the first order linear differential equation we are attempting to solve, in its standard form:

Transfer function and the Laplace transformation

Midterm exam 2, April 7, 2009 (solutions)

( ) 2! l p. Nonlinear Dynamics for Gear Fault Level. ( ) f ( x) ( ),! = sgn % " p. Open Access. Su Xunwen *,1, Liu Jinhao 1 and Wang Shaoping 2. !

On the Speed of Heat Wave. Mihály Makai

Elementary Differential Equations and Boundary Value Problems

7.4 QUANTUM MECHANICAL TREATMENT OF FLUCTUATIONS *

An Indian Journal FULL PAPER. Trade Science Inc. A stage-structured model of a single-species with density-dependent and birth pulses ABSTRACT

Frequency Response. Lecture #12 Chapter 10. BME 310 Biomedical Computing - J.Schesser

3+<6,&6([DP. September 29, SID (last 5 digits): --

d 1 = c 1 b 2 - b 1 c 2 d 2 = c 1 b 3 - b 1 c 3

Chapter 5 Digital PID control algorithm. Hesheng Wang Department of Automation,SJTU 2016,03

Institute of Actuaries of India

ECE 145A / 218 C, notes set 1: Transmission Line Properties and Analysis

On the Derivatives of Bessel and Modified Bessel Functions with Respect to the Order and the Argument

Dynamic Effects of Feedback Control!

Problem 2. Describe the following signals in terms of elementary functions (δ, u,r, ) and compute. x(t+2) x(2-t) RT_1[x] -3-2 = 1 2 = 1

fiziks Institute for NET/JRF, GATE, IIT JAM, JEST, TIFR and GRE in PHYSICAL SCIENCES MATEMATICAL PHYSICS SOLUTIONS are

EE 350 Signals and Systems Spring 2005 Sample Exam #2 - Solutions

Lab 10: RC, RL, and RLC Circuits

4.3 Design of Sections for Flexure (Part II)

More on FT. Lecture 10 4CT.5 3CT.3-5,7,8. BME 333 Biomedical Signals and Systems - J.Schesser

Sinusoidal Response Notes

MATH 308: Diff Eqs, BDP10 EXAMPLES [Belmonte, 2019] 1 Introduction 1.1 Basic Mathematical Models; Direction Fields

Linear Systems Analysis in the Time Domain

RC, RL and RLC circuits

A THREE COMPARTMENT MATHEMATICAL MODEL OF LIVER

CHE302 LECTURE VI DYNAMIC BEHAVIORS OF REPRESENTATIVE PROCESSES. Professor Dae Ryook Yang

Some Basic Information about M-S-D Systems

6.003 Homework #8 Solutions

2008 AP Calculus BC Multiple Choice Exam

Logistic equation of Human population growth (generalization to the case of reactive environment).

LAPLACE TRANSFORM AND TRANSFER FUNCTION

On General Solutions of First-Order Nonlinear Matrix and Scalar Ordinary Differential Equations

Wave Equation (2 Week)

INC 693, 481 Dynamics System and Modelling: Linear Graph Modeling II Dr.-Ing. Sudchai Boonto Assistant Professor

Section 2: The Z-Transform

10. The Discrete-Time Fourier Transform (DTFT)

CHAPTER 9. Compressible Flow. Btu ft-lb lbm ft-lb c p = = ft-lb slug- R. slug- R. 1 k. p p. p v p v. = ρ ρ

PRELIMINARY DEFINITIONS AND RELATIONS

ELECTRIC VELOCITY SERVO REGULATION

Revisiting what you have learned in Advanced Mathematical Analysis

10. If p and q are the lengths of the perpendiculars from the origin on the tangent and the normal to the curve

Why Laplace transforms?

Electrical Circuits. 1. Circuit Laws. Tools Used in Lab 13 Series Circuits Damped Vibrations: Energy Van der Pol Circuit

Boyce/DiPrima 9 th ed, Ch 7.8: Repeated Eigenvalues

This is an example to show you how SMath can calculate the movement of kinematic mechanisms.

3.4 Repeated Roots; Reduction of Order

EE 435 Lecture 42. Phased Locked Loops and VCOs

Solution: APPM 1360 Final (150 pts) Spring (60 pts total) The following parts are not related, justify your answers:

Section 3.8, Mechanical and Electrical Vibrations

University of Cyprus Biomedical Imaging and Applied Optics. Appendix. DC Circuits Capacitors and Inductors AC Circuits Operational Amplifiers

Section 5 Exercises, Problems, and Solutions. Exercises:

Q1) [20 points] answer for the following questions (ON THIS SHEET):

RESONANT CAVITY. Supplementary Instructions

Homework: Introduction to Motion

Instructors Solution for Assignment 3 Chapter 3: Time Domain Analysis of LTIC Systems

555 Timer. Digital Electronics

Solutions to FINAL JEE MAINS/IITJEE

Laplace Transforms recap for ccts

UNSTEADY FLOW OF A FLUID PARTICLE SUSPENSION BETWEEN TWO PARALLEL PLATES SUDDENLY SET IN MOTION WITH SAME SPEED

Reliability Analysis of a Bridge and Parallel Series Networks with Critical and Non- Critical Human Errors: A Block Diagram Approach.

Module 4: Time Response of discrete time systems Lecture Note 2

Examples of Dynamic Programming Problems

where: u: input y: output x: state vector A, B, C, D are const matrices

Lecture 13 RC/RL Circuits, Time Dependent Op Amp Circuits

Viscous Damping Summary Sheet No Damping Case: Damped behaviour depends on the relative size of ω o and b/2m 3 Cases: 1.

Gaussian minimum shift keying systems with additive white Gaussian noise

Transcription:

Conrol Sysm Enginring (EE0T) Assignmn: PART-A (Tim Domain Analysis: Transin Rspons Analysis). Oain h rspons of a uniy fdack sysm whos opn-loop ransfr funcion is (s) s ( s 4) for a uni sp inpu and also calcula Damping raio, Ovrshoo, sling im a ±% and ±5% olranc.. Opn loop ransfr funcion of uniy fdack sysm is (s) whr and T ar s( Ts) consans. Drmin facor y which gain should muliplid so ha ovrshoo of uni sp rspons rducd from 75% o 5%.. Th opn loop ransfr funcion of uniy fdack sysm is (s). For his sysm s Ts ( ) T ovrshoo rducd from 0.6 o 0. du o chang in only. Show ha 4. T whr and ar valus of for 0.6 and 0. ovrshoo rspcivly. 4. Th lock diagram of a simpl srvo sysm is shown in h following figur. Drmin h characrisic quaion of h sysm. Hnc calcula h undampd frquncy of oscillaions, damping raio, damping facor, maximum ovrshoo, firs undrshoo, im inrvals afr which maximum and minimum occurs, sling im and h numr of cycls compld for h oupu is sld wihin % of h final valu. Th inpu o h sysm is a uni sp. 0. 5(s )(0.s ) C( s) 5. A scond ordr conrol sysm is rprsnd y a ransfr funcion is givn y Q T 0( s) ( s) Js fs Whr Q 0 (s) is h proporional oupu and T is h inpu orqu. A sp inpu 0N-m is applid o h sysm and s rsuls ar givn as M p 6%, T p s, h sady sa oupu of h sysm is 0.5 radian. Drmin h valu of J,, and f. 6. A sysm has 40% ovrshoo and rquirs a sling im of 4 sc whn givn a sp inpu. Th sady sa rror is %. Drmin h ransfr funcion of h scond ordr sysm. Also find ris im and pak im. 7. A sandard scond ordr sysm has 50% ovrshoo and sling im of sconds. Drmin ω n, ξ, T p and T r. 5 6 Prpard y: Mr. Saish Choudhury (Ass. Profssor, Dp. of. EICE Pag of 5 W: www.schoudhury.n Email: saish@schoudhury.n, saishchoudhury@soaunivrsiy.ac.in

Conrol Sysm Enginring (EE0T) Assignmn: 8. For a uniy fdack conrol sysm having (s), find h following: s(st ) i.th facor y which h gain mus muliplid so ha h damping raio incrass from 0. o 0.9. ii.th facor y which h im consan T mus muliplid so ha h damping raio dcrass from 0.9 o 0.. T iii.show ha. 9 whn h sysm ovrshoo rducs from 70% o 0% whr and T ar valus of for 70% and 0% ovrshoo. 9. Th figur shown low shows h sp rspons of a scond ordr sysm for an inpu u(). Assuming uniy fdack, drmin ξ, ω n and opn loop ransfr funcion of h sysm. C().5.0 0.8 Tim (sc) 0. A uniy fdack sysm has h loop ransfr funcion (s). If is im rspons o hav an s s a ( ) ovrshoo of lss han 5% and sling im no xcding 4 sconds, drmin suial valus for and a.. A uniy fdack sysm is characrizd y a opn loop ransfr funcion (s). 0) Drmin h gain so ha h sysm will hav a damping raio of 5.0. For his valu of drmin sling im, pak ovrshoo and im o pak ovrshoo for a uni sp inpu.. Find pak im, sling im, and prcnag of ovrshoo for h approxima scond ordr rspons C() 0.009804 0.000857 0.009990 cos(9.796) 0.0094 5. sin(9.796). 4. A uniy fdack conrol sysm has an opn loop ransfr funcion (s). Drmin h ) ris im, pak im, pak ovrshoo, % of ovrshoo and h sling im whn a sp displacmn of 5 is givn o h sysm. 4. Drmin h valus of and T of h closd loop sysm shown in figur low, so ha h maximum ovrshoo in uni sp rspons is 0% and h pak im is.5s. Assum ha Jkg-m. Prpard y: Mr. Saish Choudhury (Ass. Profssor, Dp. of. EICE Pag of 5 W: www.schoudhury.n Email: saish@schoudhury.n, saishchoudhury@soaunivrsiy.ac.in

Conrol Sysm Enginring (EE0T) Assignmn: Js C( s) Ts 5. Drmin h sling im for h sysm givn in Q. for 4%, 6%, 9%. 6. A posiion conrol sysm is sailizd y mans of acclraion fdack. If h sysm has a momn of inria of 0-5 g-m ; viscous fricional orqu of 0-4 Nm/rad/sc and h moor orqu is givn y dθ0 dθ0 Tm 4 0 N m, whr θi θ0; Acclraion fdack d d i. Draw is lock diagram ii. Drmin h valu of for criical damping iii. Drmin h sady sa rror ss whn h inpu is a consan vlociy of 0rpm. PART-B (Tim Domain Analysis: Sady sa Analysis). Drmin h sp, ramp and paraolic rror consans of h following uniy fdack conrol sysms. Th opn loop ransfr funcions ar givn 00 ( s) ( 0.s)( 0s) s(s (s) s (s 00 00, 0s 00) s( 0.s)( 0.5s) 00 000 ( s)( 4s) 0s 00) 0)(s 00) s (s s ). Calcula saic rror cofficin for a uniy fdack sysm wih 6 (s).if inpu givn is ) r () 4 hn drmin sady sa rror. For h aov sysm of ss o rducd o 0% of xising valu, wha would h prcnag chang in gain?. Find rror cofficins for h givn uniy fdack sysm having 4. A uniy fdack conrol sysm has 4(s 0s 00) (s). )(s s 0) 0(s 4) (s), if inpu )(s s ) h sysm hn drmin h sady sa rror of h sysm. 5. A uniy fdack conrol sysm has (s) )(s s 5) i. For a uni ramp inpu i is dsird ha ss 0.. Drmin minimum valu of. ii. Drmin ss if inpu r() 4. Assum 0. r() 6 is givn o Prpard y: Mr. Saish Choudhury (Ass. Profssor, Dp. of. EICE Pag of 5 W: www.schoudhury.n Email: saish@schoudhury.n, saishchoudhury@soaunivrsiy.ac.in

Conrol Sysm Enginring (EE0T) Assignmn: 6. Using gnralizd rror sris calcula h sady-sa rror of uniy fdack sysm has 0 (s) for h following xciaion: s i. r () ii. r () iii. r() & iv. r() 7. Using gnralizd rror sris drmin h sady-sa rror of h sysm for h inpu r() 5. s s 5 00 0.5 s s C(s) 5(s ) 8. An opn loop ransfr funcion of a uniy fdack conrol sysm is (s). Using h (s )(s ) gnralizd rror sris, drmin h rror signal and sady sa rror of h sysm whn i is xcid y i. r () ii. r () iii. r() & iv. r() 9. Considr a uniy fdack conrol sysm wih h closd loop ransfr funcion C(s) R(s) s. s as Drmin h opn loop ransfr funcion (s). Show ha h sady sa rror in h uni-ramp a rspons is givn y. 0. Th figur low shows a closd loop conrol sysm which rgulas h gnraor rminal volag E 0. Th valus of and H ar 0 and 0.. Drmin h following i. Th valu of E r o kp E 0 60V. ii. Th prcnag chang in h gnraor rminal volag if h forward pah gain rducs y %. Find h rsuls (i) and (ii) whn h sysm is opn loop and closd loop. ****ALL THE BEST**** Prpard y: Mr. Saish Choudhury (Ass. Profssor, Dp. of. EICE Pag 4 of 5 W: www.schoudhury.n Email: saish@schoudhury.n, saishchoudhury@soaunivrsiy.ac.in

Conrol Sysm Enginring (EE0T) Assignmn:. C().5 0.5 Answrs (Par-A). 9.6., 4 6 4. 5rad/sc, 0.6, 4rad/sc, 9.5%, 0.94%, 0.785sc,.57sc,.sc, 0.85scs. 5..8gm, 6.4Nm/rad/sc 6. 0.5409, 0.96 7. 6.9, 0.54, 0.597, 0.958 8., 9 9 9. 0.495, 0.rad/sc, 4.98) 0., a. 00, 0.8, 6.%, 0.6. sc, 0.07, 0., 5.66%..9,.8,.445, 6.%, 4sc (±%), sc (±5%) 4. 5.54, T0.88 5. Answr no givn 6..4 0 sc, ο Answrs (Par-B). ( 000,0,0),(,,0),(,0),( ),( 0),( )., ss.5 p v 40.,0 4. 5. 50, 4 0 6. () 0. 5 () () 7 7. () 0.04 0.66 0.05 8. Answr no givn 9. Answr no givn 0..8V,.8V, %, 0.495% 0 44 78 () 0.98 0.40 0.08 Prpard y: Mr. Saish Choudhury (Ass. Profssor, Dp. of. EICE Pag 5 of 5 W: www.schoudhury.n Email: saish@schoudhury.n, saishchoudhury@soaunivrsiy.ac.in