I ml. g l. sin. l 0,,2,...,n A. ( t vs. ), and ( vs. ). d dt. sin l
|
|
- Shannon White
- 5 years ago
- Views:
Transcription
1 Advanced Control Theory Homework #3 Student No.597 Name : Jinseong Kim. The simple pendulum dynamics is given by g sin L A. Derive above dynamic equation from the free body diagram. B. Find the equilibrium point of the simple pendulum. C. Linearize above system with respect to each equilibrium point. Express in the form of x( t. Ax D. Simulate the original and linearized system with Runge-Kutta 4 th order. Draw the graph of ( t vs., ( t vs., and ( vs.. - Solution A. Free body diagram은아래그림과같이그렸다. T I lf lmgsin where, I ml B. g l sin 문제와같은식을얻으려면 의기준을 3 시방향으로잡으면된다. For the equilibrium points, we must solve d f ( g dt sin l g and sin l,,,...,n C. D. f f x x A g g f f cos l l x x Case study - (with l.5, g 9.8, =, =.3
2 Advanced Control Theory Homework #3 Student No.597 Name : Jinseong Kim Case study - (with l.5, g 9.8, =, =.. For the following nonlinear input-output system y( t y( y ( y uu A. Obtain a nonlinear state-space representation. B. Linearize this system around its equilibrium output trajectory when u(, and write it in state space form. C. Simulate the original and linearized system with Runge-Kutta 4 th order. Draw the graph of ( t vs. y, ( t vs. y, and ( y vs. y. - Solution A. d y y dt y y y y y yuu B. For the equilibrium points, we must solve y f( y y y y y yuu y yy y y y u u y y ( y(y y u(, y Linearize using the Jacobian f f y y A f f yy y y y, y y y f f u u B f f y, y u u State space form
3 ECE 55, Fall 5 Problem Set # Solution Solutions: (Remember: generally, there are more than one state-space realizations of the same system.. Nonlinear system ( points (a A straightforward attempt is to denote x = y and x = ẏ, then one can write { x = x, x = ÿ = x (x + (x + + u + u. The main problem in defining the state variables in this case lies in the derivative terms of the input signal u. The state variables must be such that they will eliminate the derivatives of u in the state equation. One way to obtain a correct equation is to define (by direct examination of the given equation: x = y, x = x u. Hence the corresponding state-space equations are x = ẏ = x + u, x = ẍ u = ÿ u = x (x + (x + u + + u, y = x. A more systematic way to obtain the state-space equation is using the integration technique (compare to picking state variables by direct examination. From ÿ = y (y + (ẏ + + u + u, integrate to obtain ẏ = u + (y + u (y + (ẏ +. Let x = (y +u (y +(ẏ +. Then ẏ = u+x and ẋ = (y +u (y +(ẏ +. Let x = y, then we have a state-space realization { x + u which is the same as (. ẋ = x (x + (x + u + + u (b The first step is to obtain its equilibrium. Set u and x, x in equation (, and we have { { x = x (x + (x + = x (x + = x = x = Linearize the system ( at (,, and we get ( ( f f δ δx + x u x=(, u= δy = [ δx. x=(, u= δu = [ [ δx + δu, 3 (
4 . Satellite Problem ( points Note, in the system: r = r θ k r + u ( θ = θṙ r + r u (3 that θ does not explicitly appear in the equations. Hence we may pick the states to be x = [x, x, x 3 T = [ṙ, r, θ T R 3 and denote the inputs to be u = [u, u T R. The state space representation of the system is: r ṙ θ = f (ṙ, r, θ, u, u f (ṙ, r, θ, u, u f 3 (ṙ, r, θ, u, u = r θ k/r + u ṙ θṙ/r + u /r (4 Then f x = f ṙ f ṙ f 3 ṙ f r f r f 3 r f f θ f θ 3 θ = θ + k/r 3 r θ θ/r θṙ/r u /r ṙr = 3ω pω ω/p evaluated at ṙ =, r = p, θ = ω, u = u = and k = p 3 ω. Similarly we have: f u =. (5 /p The linearized equation is therefore: 3ω pω δ ω/p δx + /p δu. (6 3. A Multiple Input and Multiple Output (MIMO System ( points Assume that the system is relaxed at t =. Then integrate the differential equations to obtain: ẏ = u + ( y + u + ( 3y + u (7 ẏ = ( y + 3y + u 3 + ( y y + u u 3 (8 Denote the inputs to be u = [u, u, u 3 T R 3 and the outputs y = [y, y T R. Define the state variables to be x = [x, x, x 3, x 4, x 5 T R 5 where: x = y, x = ( y + u + x 3, x 3 = ( 3y + u, x 4 = y, x 5 = ( y y + u u 3.
5 Then the state equations are: Or in matrix form: y = ẋ = x + u ẋ = x + x 3 + u ẋ 3 = 3x 4 + u ẋ 4 = x + 3x 4 + x 5 + u 3 ẋ 5 = x x 4 + u u 3 y = x y = x [ x + u (9 x ( 4. A Linear Time Varying System ( points (a Let us first assume that the system is relaxed at time t =, integrate the system and we get: ÿ ẏ y = t u + (t + u ẏ = (y + tu + t (y + τu dτ. ( Now let x = [x, x T R where we define x = y and x = t (y + τu dτ = ẏ y tu. Then we have: [ [ t x + u t y = [ ( x (b Define w = tu. Then ÿ ẏ y = w + ẇ, which is a linear system with input w and output y. So, the transfer function is Y (s W (s = s + s s, which gives the state space in the controllable canonical form: [ [ [ [ x + w = x + t y = [ x. u (3 3
6 In fact, the state-space in part (a is the observable canonical form with respect to input w and output y. Yet another solution: Let x = y, x = ẏ tu. Then ( ( ẏ x = + tu = ÿ t u u x + x + 3tu y = [ x 5. State-space vs. Input-output Representation ( points For the given transfer function, we have: G(s = [ [ t x + u 3t (4 s + s 3 + 4s + 5s + = s + (s + (s + = B(s A(s. (5 (a Controllable canonical form. Let A(sW (s = U(s, Y (s = B(sW (s, i.e. w (3 + 4ẅ + 5ẇ + w = u and y = ẇ + w. Choose the states to be x = [w, ẇ, ẅ T R 3. Then we have x + u 5 4 y = [ x (b Observable canonical form. From y (3 + 4ÿ + 5ẏ + y = u + u we define the states to be x = [x, x, x 3 T : x = y x = ẏ + 4y x 3 = ÿ + 4ẏ + 5y u Then we obtain: 4 5 y = [ x x + u (c Using partial fractions, we have: s + (s + (s + = = (s + (s + = A (s + + A (s + (s + + (s + Let X (s = (s+ U(s, X (s = (s+ U(s, then Y (s = X (s X (s, or in the time domain: [ y = [ x x + [ u 4
HW 6 Mathematics 503, Mathematical Modeling, CSUF, June 24, 2007
HW 6 Mathematics 503, Mathematical Modeling, CSUF, June 24, 2007 Nasser M. Abbasi June 15, 2014 Contents 1 Problem 1 (section 3.5,#9, page 197 1 2 Problem 1 (section 3.5,#9, page 197 7 1 Problem 1 (section
More information2.10 Saddles, Nodes, Foci and Centers
2.10 Saddles, Nodes, Foci and Centers In Section 1.5, a linear system (1 where x R 2 was said to have a saddle, node, focus or center at the origin if its phase portrait was linearly equivalent to one
More informationSolutions to Dynamical Systems 2010 exam. Each question is worth 25 marks.
Solutions to Dynamical Systems exam Each question is worth marks [Unseen] Consider the following st order differential equation: dy dt Xy yy 4 a Find and classify all the fixed points of Hence draw the
More informationM2A2 Problem Sheet 3 - Hamiltonian Mechanics
MA Problem Sheet 3 - Hamiltonian Mechanics. The particle in a cone. A particle slides under gravity, inside a smooth circular cone with a vertical axis, z = k x + y. Write down its Lagrangian in a) Cartesian,
More informationLinearization problem. The simplest example
Linear Systems Lecture 3 1 problem Consider a non-linear time-invariant system of the form ( ẋ(t f x(t u(t y(t g ( x(t u(t (1 such that x R n u R m y R p and Slide 1 A: f(xu f(xu g(xu and g(xu exist and
More informationMAE 143B - Homework 8 Solutions
MAE 43B - Homework 8 Solutions P6.4 b) With this system, the root locus simply starts at the pole and ends at the zero. Sketches by hand and matlab are in Figure. In matlab, use zpk to build the system
More informationControl Systems I. Lecture 2: Modeling. Suggested Readings: Åström & Murray Ch. 2-3, Guzzella Ch Emilio Frazzoli
Control Systems I Lecture 2: Modeling Suggested Readings: Åström & Murray Ch. 2-3, Guzzella Ch. 2-3 Emilio Frazzoli Institute for Dynamic Systems and Control D-MAVT ETH Zürich September 29, 2017 E. Frazzoli
More informationReview: control, feedback, etc. Today s topic: state-space models of systems; linearization
Plan of the Lecture Review: control, feedback, etc Today s topic: state-space models of systems; linearization Goal: a general framework that encompasses all examples of interest Once we have mastered
More informationTopic # Feedback Control
Topic #7 16.31 Feedback Control State-Space Systems What are state-space models? Why should we use them? How are they related to the transfer functions used in classical control design and how do we develop
More information9 11 Solve the initial-value problem Evaluate the integral. 1. y sin 3 x cos 2 x dx. calculation. 1 + i i23
Mock Exam 1 5 8 Solve the differential equation. 7. d dt te t s1 Mock Exam 9 11 Solve the initial-value problem. 9. x ln x, 1 3 6 Match the differential equation with its direction field (labeled I IV).
More informationComputational Physics (6810): Session 8
Computational Physics (6810): Session 8 Dick Furnstahl Nuclear Theory Group OSU Physics Department February 24, 2014 Differential equation solving Session 7 Preview Session 8 Stuff Solving differential
More information4 Second-Order Systems
4 Second-Order Systems Second-order autonomous systems occupy an important place in the study of nonlinear systems because solution trajectories can be represented in the plane. This allows for easy visualization
More informationAnalytical Mechanics: Variational Principles
Analytical Mechanics: Variational Principles Shinichi Hirai Dept. Robotics, Ritsumeikan Univ. Shinichi Hirai (Dept. Robotics, Ritsumeikan Univ.) Analytical Mechanics: Variational Principles 1 / 71 Agenda
More informationStability of Nonlinear Systems An Introduction
Stability of Nonlinear Systems An Introduction Michael Baldea Department of Chemical Engineering The University of Texas at Austin April 3, 2012 The Concept of Stability Consider the generic nonlinear
More informationPractice Problems for Final Exam
Math 1280 Spring 2016 Practice Problems for Final Exam Part 2 (Sections 6.6, 6.7, 6.8, and chapter 7) S o l u t i o n s 1. Show that the given system has a nonlinear center at the origin. ẋ = 9y 5y 5,
More informationE209A: Analysis and Control of Nonlinear Systems Problem Set 6 Solutions
E9A: Analysis and Control of Nonlinear Systems Problem Set 6 Solutions Michael Vitus Gabe Hoffmann Stanford University Winter 7 Problem 1 The governing equations are: ẋ 1 = x 1 + x 1 x ẋ = x + x 3 Using
More informationfor changing independent variables. Most simply for a function f(x) the Legendre transformation f(x) B(s) takes the form B(s) = xs f(x) with s = df
Physics 106a, Caltech 1 November, 2018 Lecture 10: Hamiltonian Mechanics I The Hamiltonian In the Hamiltonian formulation of dynamics each second order ODE given by the Euler- Lagrange equation in terms
More informationNonlinear Oscillators: Free Response
20 Nonlinear Oscillators: Free Response Tools Used in Lab 20 Pendulums To the Instructor: This lab is just an introduction to the nonlinear phase portraits, but the connection between phase portraits and
More informationCDS 101 Precourse Phase Plane Analysis and Stability
CDS 101 Precourse Phase Plane Analysis and Stability Melvin Leok Control and Dynamical Systems California Institute of Technology Pasadena, CA, 26 September, 2002. mleok@cds.caltech.edu http://www.cds.caltech.edu/
More information+ i. cos(t) + 2 sin(t) + c 2.
MATH HOMEWORK #7 PART A SOLUTIONS Problem 7.6.. Consider the system x = 5 x. a Express the general solution of the given system of equations in terms of realvalued functions. b Draw a direction field,
More informationControl Systems I. Lecture 2: Modeling and Linearization. Suggested Readings: Åström & Murray Ch Jacopo Tani
Control Systems I Lecture 2: Modeling and Linearization Suggested Readings: Åström & Murray Ch. 2-3 Jacopo Tani Institute for Dynamic Systems and Control D-MAVT ETH Zürich September 28, 2018 J. Tani, E.
More informationPhysics 5153 Classical Mechanics. Canonical Transformations-1
1 Introduction Physics 5153 Classical Mechanics Canonical Transformations The choice of generalized coordinates used to describe a physical system is completely arbitrary, but the Lagrangian is invariant
More informationMore Examples Of Generalized Coordinates
Slides of ecture 8 Today s Class: Review Of Homework From ecture 7 Hamilton s Principle More Examples Of Generalized Coordinates Calculating Generalized Forces Via Virtual Work /3/98 /home/djsegal/unm/vibcourse/slides/ecture8.frm
More informationTwo dimensional oscillator and central forces
Two dimensional oscillator and central forces September 4, 04 Hooke s law in two dimensions Consider a radial Hooke s law force in -dimensions, F = kr where the force is along the radial unit vector and
More information1. < 0: the eigenvalues are real and have opposite signs; the fixed point is a saddle point
Solving a Linear System τ = trace(a) = a + d = λ 1 + λ 2 λ 1,2 = τ± = det(a) = ad bc = λ 1 λ 2 Classification of Fixed Points τ 2 4 1. < 0: the eigenvalues are real and have opposite signs; the fixed point
More information8 Example 1: The van der Pol oscillator (Strogatz Chapter 7)
8 Example 1: The van der Pol oscillator (Strogatz Chapter 7) So far we have seen some different possibilities of what can happen in two-dimensional systems (local and global attractors and bifurcations)
More informationSystems of Linear ODEs
P a g e 1 Systems of Linear ODEs Systems of ordinary differential equations can be solved in much the same way as discrete dynamical systems if the differential equations are linear. We will focus here
More information1 Controllability and Observability
1 Controllability and Observability 1.1 Linear Time-Invariant (LTI) Systems State-space: Dimensions: Notation Transfer function: ẋ = Ax+Bu, x() = x, y = Cx+Du. x R n, u R m, y R p. Note that H(s) is always
More informationMATH 44041/64041 Applied Dynamical Systems, 2018
MATH 4441/6441 Applied Dynamical Systems, 218 Answers to Assessed Coursework 1 1 Method based on series expansion of the matrix exponential Let the coefficient matrix of α the linear system be A, then
More informationCHALMERS, GÖTEBORGS UNIVERSITET. EXAM for DYNAMICAL SYSTEMS. COURSE CODES: TIF 155, FIM770GU, PhD
CHALMERS, GÖTEBORGS UNIVERSITET EXAM for DYNAMICAL SYSTEMS COURSE CODES: TIF 155, FIM770GU, PhD Time: Place: Teachers: Allowed material: Not allowed: April 06, 2018, at 14 00 18 00 Johanneberg Kristian
More informationTopic # /31 Feedback Control Systems. Analysis of Nonlinear Systems Lyapunov Stability Analysis
Topic # 16.30/31 Feedback Control Systems Analysis of Nonlinear Systems Lyapunov Stability Analysis Fall 010 16.30/31 Lyapunov Stability Analysis Very general method to prove (or disprove) stability of
More information2 Lyapunov Stability. x(0) x 0 < δ x(t) x 0 < ɛ
1 2 Lyapunov Stability Whereas I/O stability is concerned with the effect of inputs on outputs, Lyapunov stability deals with unforced systems: ẋ = f(x, t) (1) where x R n, t R +, and f : R n R + R n.
More informationSTABILITY. Phase portraits and local stability
MAS271 Methods for differential equations Dr. R. Jain STABILITY Phase portraits and local stability We are interested in system of ordinary differential equations of the form ẋ = f(x, y), ẏ = g(x, y),
More information1 Lyapunov theory of stability
M.Kawski, APM 581 Diff Equns Intro to Lyapunov theory. November 15, 29 1 1 Lyapunov theory of stability Introduction. Lyapunov s second (or direct) method provides tools for studying (asymptotic) stability
More informationSystem Control Engineering
System Control Engineering 0 Koichi Hashimoto Graduate School of Information Sciences Text: Feedback Systems: An Introduction for Scientists and Engineers Author: Karl J. Astrom and Richard M. Murray Text:
More informationChapter 1: Introduction
Chapter 1: Introduction Definition: A differential equation is an equation involving the derivative of a function. If the function depends on a single variable, then only ordinary derivatives appear and
More informationIn the presence of viscous damping, a more generalized form of the Lagrange s equation of motion can be written as
2 MODELING Once the control target is identified, which includes the state variable to be controlled (ex. speed, position, temperature, flow rate, etc), and once the system drives are identified (ex. force,
More informationEECS C128/ ME C134 Final Wed. Dec. 15, am. Closed book. Two pages of formula sheets. No calculators.
Name: SID: EECS C28/ ME C34 Final Wed. Dec. 5, 2 8- am Closed book. Two pages of formula sheets. No calculators. There are 8 problems worth points total. Problem Points Score 2 2 6 3 4 4 5 6 6 7 8 2 Total
More information2 We imagine that our double pendulum is immersed in a uniform downward directed gravitational field, with gravitational constant g.
THE MULTIPLE SPHERICAL PENDULUM Thomas Wieting Reed College, 011 1 The Double Spherical Pendulum Small Oscillations 3 The Multiple Spherical Pendulum 4 Small Oscillations 5 Linear Mechanical Systems 1
More informationA plane autonomous system is a pair of simultaneous first-order differential equations,
Chapter 11 Phase-Plane Techniques 11.1 Plane Autonomous Systems A plane autonomous system is a pair of simultaneous first-order differential equations, ẋ = f(x, y), ẏ = g(x, y). This system has an equilibrium
More informationLogistic Map, Euler & Runge-Kutta Method and Lotka-Volterra Equations
Logistic Map, Euler & Runge-Kutta Method and Lotka-Volterra Equations S. Y. Ha and J. Park Department of Mathematical Sciences Seoul National University Sep 23, 2013 Contents 1 Logistic Map 2 Euler and
More informationHigh-Gain Observers in Nonlinear Feedback Control. Lecture # 2 Separation Principle
High-Gain Observers in Nonlinear Feedback Control Lecture # 2 Separation Principle High-Gain ObserversinNonlinear Feedback ControlLecture # 2Separation Principle p. 1/4 The Class of Systems ẋ = Ax + Bφ(x,
More informationExam 2 Study Guide: MATH 2080: Summer I 2016
Exam Study Guide: MATH 080: Summer I 016 Dr. Peterson June 7 016 First Order Problems Solve the following IVP s by inspection (i.e. guessing). Sketch a careful graph of each solution. (a) u u; u(0) 0.
More information1 The pendulum equation
Math 270 Honors ODE I Fall, 2008 Class notes # 5 A longer than usual homework assignment is at the end. The pendulum equation We now come to a particularly important example, the equation for an oscillating
More informationYou may hold onto this portion of the test and work on it some more after you have completed the no calculator portion of the test.
MTH 5 Winter Term 010 Test 1- Calculator Portion Name You may hold onto this portion of the test and work on it some more after you have completed the no calculator portion of the test. 1. Consider the
More informationDifferential equations, comprehensive exam topics and sample questions
Differential equations, comprehensive exam topics and sample questions Topics covered ODE s: Chapters -5, 7, from Elementary Differential Equations by Edwards and Penney, 6th edition.. Exact solutions
More informationEE222 - Spring 16 - Lecture 2 Notes 1
EE222 - Spring 16 - Lecture 2 Notes 1 Murat Arcak January 21 2016 1 Licensed under a Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International License. Essentially Nonlinear Phenomena Continued
More informationConsider a particle in 1D at position x(t), subject to a force F (x), so that mẍ = F (x). Define the kinetic energy to be.
Chapter 4 Energy and Stability 4.1 Energy in 1D Consider a particle in 1D at position x(t), subject to a force F (x), so that mẍ = F (x). Define the kinetic energy to be T = 1 2 mẋ2 and the potential energy
More informationPHY 5246: Theoretical Dynamics, Fall November 16 th, 2015 Assignment # 11, Solutions. p θ = L θ = mr2 θ, p φ = L θ = mr2 sin 2 θ φ.
PHY 5246: Theoretical Dynamics, Fall 215 November 16 th, 215 Assignment # 11, Solutions 1 Graded problems Problem 1 1.a) The Lagrangian is L = 1 2 m(ṙ2 +r 2 θ2 +r 2 sin 2 θ φ 2 ) V(r), (1) and the conjugate
More informationA Model of Evolutionary Dynamics with Quasiperiodic Forcing
paper presented at Society for Experimental Mechanics (SEM) IMAC XXXIII Conference on Structural Dynamics February 2-5, 205, Orlando FL A Model of Evolutionary Dynamics with Quasiperiodic Forcing Elizabeth
More informationInverse Kinematics. Mike Bailey.
Inverse Kinematics This work is licensed under a Creative Commons Attribution-NonCommercial- NoDerivatives 4.0 International License Mike Bailey mjb@cs.oregonstate.edu inversekinematics.pptx Inverse Kinematics
More informationECE 602 Solution to Homework Assignment 1
ECE 6 Solution to Assignment 1 December 1, 7 1 ECE 6 Solution to Homework Assignment 1 1. For a function to be linear, it must satisfy y = f() = in addition to y = ax, so only the first graph represents
More informationMath 216 Final Exam 14 December, 2012
Math 216 Final Exam 14 December, 2012 This sample exam is provided to serve as one component of your studying for this exam in this course. Please note that it is not guaranteed to cover the material that
More informationSolutions: Homework 2 Biomedical Signal, Systems and Control (BME )
Solutions: Homework 2 Biomedical Signal, Systems and Control (BE 580.222) Instructor: René Vidal, E-mail: rvidal@cis.jhu.edu TA: Donavan Cheng, E-mail: donavan.cheng@gmail.com TA: Ertan Cetingül, E-mail:
More informationPHYSICS 1 Simple Harmonic Motion
Advanced Placement PHYSICS 1 Simple Harmonic Motion Student 014-015 What I Absolutely Have to Know to Survive the AP* Exam Whenever the acceleration of an object is proportional to its displacement and
More informationTo explore and investigate projectile motion and how it can be applied to various problems.
NAME: ΔY = 0 Projectile Motion Computer Lab Purpose: To explore and investigate projectile motion and how it can be applied to various problems. Procedure: 1. First, go to the following web site http://galileoandeinstein.physics.virginia.edu/more_stuff/applets/projectile
More informationPHY6426/Fall 07: CLASSICAL MECHANICS HOMEWORK ASSIGNMENT #1 due by 9:35 a.m. Wed 09/05 Instructor: D. L. Maslov Rm.
PHY646/Fall 07: CLASSICAL MECHANICS HOMEWORK ASSIGNMENT # due by 9:35 a.m. Wed 09/05 Instructor: D. L. Maslov maslov@phys.ufl.edu 39-053 Rm. 4 Please help your instructor by doing your work neatly.. Goldstein,
More informationCP1 REVISION LECTURE 3 INTRODUCTION TO CLASSICAL MECHANICS. Prof. N. Harnew University of Oxford TT 2017
CP1 REVISION LECTURE 3 INTRODUCTION TO CLASSICAL MECHANICS Prof. N. Harnew University of Oxford TT 2017 1 OUTLINE : CP1 REVISION LECTURE 3 : INTRODUCTION TO CLASSICAL MECHANICS 1. Angular velocity and
More informationNon-Linear Dynamics Homework Solutions Week 6
Non-Linear Dynamics Homework Solutions Week 6 Chris Small March 6, 2007 Please email me at smachr09@evergreen.edu with any questions or concerns reguarding these solutions. 6.8.3 Locate annd find the index
More informationDepartment of Aerospace Engineering and Mechanics University of Minnesota Written Preliminary Examination: Control Systems Friday, April 9, 2010
Department of Aerospace Engineering and Mechanics University of Minnesota Written Preliminary Examination: Control Systems Friday, April 9, 2010 Problem 1: Control of Short Period Dynamics Consider the
More informationPhysics 6010, Fall 2016 Constraints and Lagrange Multipliers. Relevant Sections in Text:
Physics 6010, Fall 2016 Constraints and Lagrange Multipliers. Relevant Sections in Text: 1.3 1.6 Constraints Often times we consider dynamical systems which are defined using some kind of restrictions
More informationDifferential Equations: Homework 8
Differential Equations: Homework 8 Alvin Lin January 08 - May 08 Section.6 Exercise Find a general solution to the differential equation using the method of variation of parameters. y + y = tan(t) r +
More informationCalculus I Homework: Linear Approximation and Differentials Page 1
Calculus I Homework: Linear Approximation and Differentials Page Example (3..8) Find the linearization L(x) of the function f(x) = (x) /3 at a = 8. The linearization is given by which approximates the
More informationLagrangian Dynamics: Derivations of Lagrange s Equations
Constraints and Degrees of Freedom 1.003J/1.053J Dynamics and Control I, Spring 007 Professor Thomas Peacock 4/9/007 Lecture 15 Lagrangian Dynamics: Derivations of Lagrange s Equations Constraints and
More informationThe Nonlinear Pendulum
The Nonlinear Pendulum Evan Sheridan 11367741 Feburary 18th 013 Abstract Both the non-linear linear pendulum are investigated compared using the pendulum.c program that utilizes the trapezoid method for
More information154 Chapter 9 Hints, Answers, and Solutions The particular trajectories are highlighted in the phase portraits below.
54 Chapter 9 Hints, Answers, and Solutions 9. The Phase Plane 9.. 4. The particular trajectories are highlighted in the phase portraits below... 3. 4. 9..5. Shown below is one possibility with x(t) and
More information3 Space curvilinear motion, motion in non-inertial frames
3 Space curvilinear motion, motion in non-inertial frames 3.1 In-class problem A rocket of initial mass m i is fired vertically up from earth and accelerates until its fuel is exhausted. The residual mass
More informationAIMS Exercise Set # 1
AIMS Exercise Set #. Determine the form of the single precision floating point arithmetic used in the computers at AIMS. What is the largest number that can be accurately represented? What is the smallest
More informationCalculus I Homework: Linear Approximation and Differentials Page 1
Calculus I Homework: Linear Approximation and Differentials Page Questions Example Find the linearization L(x) of the function f(x) = (x) /3 at a = 8. Example Find the linear approximation of the function
More informationOHSx XM521 Multivariable Differential Calculus: Homework Solutions 14.1
OHSx XM5 Multivariable Differential Calculus: Homework Solutions 4. (8) Describe the graph of the equation. r = i + tj + (t )k. Solution: Let y(t) = t, so that z(t) = t = y. In the yz-plane, this is just
More informationLecture 5. Outline: Limit Cycles. Definition and examples How to rule out limit cycles. Poincare-Bendixson theorem Hopf bifurcations Poincare maps
Lecture 5 Outline: Limit Cycles Definition and examples How to rule out limit cycles Gradient systems Liapunov functions Dulacs criterion Poincare-Bendixson theorem Hopf bifurcations Poincare maps Limit
More informationConstraints. Noninertial coordinate systems
Chapter 8 Constraints. Noninertial codinate systems 8.1 Constraints Oftentimes we encounter problems with constraints. F example, f a ball rolling on a flo without slipping, there is a constraint linking
More informationy + 3y = 0, y(0) = 2, y (0) = 3
MATH 3 HOMEWORK #3 PART A SOLUTIONS Problem 311 Find the solution of the given initial value problem Sketch the graph of the solution and describe its behavior as t increases y + 3y 0, y(0), y (0) 3 Solution
More informationHomework 7: # 4.22, 5.15, 5.21, 5.23, Foucault pendulum
Homework 7: # 4., 5.15, 5.1, 5.3, Foucault pendulum Michael Good Oct 9, 4 4. A projectile is fired horizontally along Earth s surface. Show that to a first approximation the angular deviation from the
More informationLagrangian Analysis of 2D and 3D Ocean Flows from Eulerian Velocity Data
Flows from Second-year Ph.D. student, Applied Math and Scientific Computing Project Advisor: Kayo Ide Department of Atmospheric and Oceanic Science Center for Scientific Computation and Mathematical Modeling
More information21.60 Worksheet 8 - preparation problems - question 1:
Dynamics 190 1.60 Worksheet 8 - preparation problems - question 1: A particle of mass m moes under the influence of a conseratie central force F (r) =g(r)r where r = xˆx + yŷ + zẑ and r = x + y + z. A.
More informationClassical Mechanics Comprehensive Exam Solution
Classical Mechanics Comprehensive Exam Solution January 31, 011, 1:00 pm 5:pm Solve the following six problems. In the following problems, e x, e y, and e z are unit vectors in the x, y, and z directions,
More informationPHY321 Homework Set 10
PHY321 Homework Set 10 1. [5 pts] A small block of mass m slides without friction down a wedge-shaped block of mass M and of opening angle α. Thetriangular block itself slides along a horizontal floor,
More informationarxiv: v1 [nlin.ao] 26 Oct 2012
COMMENT ON THE ARTICLE DISTILLING FREE-FORM NATURAL LAWS FROM EXPERIMENTAL DATA CHRISTOPHER HILLAR AND FRIEDRICH T. SOMMER arxiv:1210.7273v1 [nlin.ao] 26 Oct 2012 1. Summary A paper by Schmi and Lipson
More informationEECS C128/ ME C134 Final Wed. Dec. 14, am. Closed book. One page, 2 sides of formula sheets. No calculators.
Name: SID: EECS C128/ ME C134 Final Wed. Dec. 14, 211 81-11 am Closed book. One page, 2 sides of formula sheets. No calculators. There are 8 problems worth 1 points total. Problem Points Score 1 16 2 12
More informationconditional cdf, conditional pdf, total probability theorem?
6 Multiple Random Variables 6.0 INTRODUCTION scalar vs. random variable cdf, pdf transformation of a random variable conditional cdf, conditional pdf, total probability theorem expectation of a random
More informationPhysics 351, Spring 2015, Final Exam.
Physics 351, Spring 2015, Final Exam. This closed-book exam has (only) 25% weight in your course grade. You can use one sheet of your own hand-written notes. Please show your work on these pages. The back
More informationNonlinear Control. Nonlinear Control Lecture # 2 Stability of Equilibrium Points
Nonlinear Control Lecture # 2 Stability of Equilibrium Points Basic Concepts ẋ = f(x) f is locally Lipschitz over a domain D R n Suppose x D is an equilibrium point; that is, f( x) = 0 Characterize and
More information1.11 Some Higher-Order Differential Equations
page 99. Some Higher-Order Differential Equations 99. Some Higher-Order Differential Equations So far we have developed analytical techniques only for solving special types of firstorder differential equations.
More informationEE C128 / ME C134 Final Exam Fall 2014
EE C128 / ME C134 Final Exam Fall 2014 December 19, 2014 Your PRINTED FULL NAME Your STUDENT ID NUMBER Number of additional sheets 1. No computers, no tablets, no connected device (phone etc.) 2. Pocket
More informationENGI 3424 Mid Term Test Solutions Page 1 of 9
ENGI 344 Mid Term Test 07 0 Solutions Page of 9. The displacement st of the free end of a mass spring sstem beond the equilibrium position is governed b the ordinar differential equation d s ds 3t 6 5s
More informationJUST THE MATHS UNIT NUMBER DIFFERENTIATION 3 (Elementary techniques of differentiation) A.J.Hobson
JUST THE MATHS UNIT NUMBER 10.3 DIFFERENTIATION 3 (Elementary techniques of differentiation) by A.J.Hobson 10.3.1 Standard derivatives 10.3.2 Rules of differentiation 10.3.3 Exercises 10.3.4 Answers to
More informationPhysics 351, Spring 2015, Homework #5. Due at start of class, Friday, February 20, 2015 Course info is at positron.hep.upenn.
Physics 351, Spring 2015, Homework #5. Due at start of class, Friday, February 20, 2015 Course info is at positron.hep.upenn.edu/p351 When you finish this homework, remember to visit the feedback page
More informationMath 4200, Problem set 3
Math, Problem set 3 Solutions September, 13 Problem 1. ẍ = ω x. Solution. Following the general theory of conservative systems with one degree of freedom let us define the kinetic energy T and potential
More informationTHE SEPARATRIX FOR A SECOND ORDER ORDINARY DIFFERENTIAL EQUATION OR A 2 2 SYSTEM OF FIRST ORDER ODE WHICH ALLOWS A PHASE PLANE QUANTITATIVE ANALYSIS
THE SEPARATRIX FOR A SECOND ORDER ORDINARY DIFFERENTIAL EQUATION OR A SYSTEM OF FIRST ORDER ODE WHICH ALLOWS A PHASE PLANE QUANTITATIVE ANALYSIS Maria P. Skhosana and Stephan V. Joubert, Tshwane University
More informationMATHEMATICAL MODELLING, MECHANICS AND MOD- ELLING MTHA4004Y
UNIVERSITY OF EAST ANGLIA School of Mathematics Main Series UG Examination 2017 18 MATHEMATICAL MODELLING, MECHANICS AND MOD- ELLING MTHA4004Y Time allowed: 2 Hours Attempt QUESTIONS 1 and 2, and ONE other
More informationLecture Notes for PHY 405 Classical Mechanics
Lecture Notes for PHY 405 Classical Mechanics From Thorton & Marion s Classical Mechanics Prepared by Dr. Joseph M. Hahn Saint Mary s University Department of Astronomy & Physics September 1, 2005 Chapter
More informationNonlinear Control Lecture 2:Phase Plane Analysis
Nonlinear Control Lecture 2:Phase Plane Analysis Farzaneh Abdollahi Department of Electrical Engineering Amirkabir University of Technology Fall 2010 r. Farzaneh Abdollahi Nonlinear Control Lecture 2 1/53
More informationLecture 9 Nonlinear Control Design
Lecture 9 Nonlinear Control Design Exact-linearization Lyapunov-based design Lab 2 Adaptive control Sliding modes control Literature: [Khalil, ch.s 13, 14.1,14.2] and [Glad-Ljung,ch.17] Course Outline
More informationModelling and Mathematical Methods in Process and Chemical Engineering
Modelling and Mathematical Methods in Process and Chemical Engineering Solution Series 3 1. Population dynamics: Gendercide The system admits two steady states The Jacobi matrix is ẋ = (1 p)xy k 1 x ẏ
More informationECE557 Systems Control
ECE557 Systems Control Bruce Francis Course notes, Version.0, September 008 Preface This is the second Engineering Science course on control. It assumes ECE56 as a prerequisite. If you didn t take ECE56,
More informationMEM 255 Introduction to Control Systems: Modeling & analyzing systems
MEM 55 Introduction to Control Systems: Modeling & analyzing systems Harry G. Kwatny Department of Mechanical Engineering & Mechanics Drexel University Outline The Pendulum Micro-machined capacitive accelerometer
More informationPhys 7221, Fall 2006: Midterm exam
Phys 7221, Fall 2006: Midterm exam October 20, 2006 Problem 1 (40 pts) Consider a spherical pendulum, a mass m attached to a rod of length l, as a constrained system with r = l, as shown in the figure.
More informationL = 1 2 a(q) q2 V (q).
Physics 3550, Fall 2011 Motion near equilibrium - Small Oscillations Relevant Sections in Text: 5.1 5.6 Motion near equilibrium 1 degree of freedom One of the most important situations in physics is motion
More informationLecture 38. Almost Linear Systems
Math 245 - Mathematics of Physics and Engineering I Lecture 38. Almost Linear Systems April 20, 2012 Konstantin Zuev (USC) Math 245, Lecture 38 April 20, 2012 1 / 11 Agenda Stability Properties of Linear
More information