Applications of the Wronskian and Gram Matrices of {Fie”K?
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Solutions to Math 53 Practice Second Midterm
Solutions to Math 53 Practice Second Midterm 1. (20 points) dx dy (a) (10 points) Write down the general solution to the system of equations dt = x+y; dt = −13x−3y in terms of real-valued functions. (b) (5 points) The trajectories of this equation in the (x; y)-plane rotate around the origin. Is this dx rotation clockwise or counterclockwise? If we changed the first equation to dt = −x + y, would it change the direction of rotation? (c) (5 points) Suppose (x1(t); y1(t)) and (x2(t); y2(t)) are two solutions to this equation. Define the Wronskian determinant W (t) of these two solutions. If W (0) = 1, what is W (10)? Note: the material for this part will be covered in the May 8 and May 10 lectures. 1 1 (a) The corresponding matrix is A = , with characteristic polynomial (1 − λ)(−3 − −13 −3 λ) + 13 = 0, so that λ2 + 2λ + 10 = 0, so that λ = −1 ± 3i. The corresponding eigenvector v to λ1 = −1 + 3i must be a solution to 2 − 3i 1 −13 −2 − 3i 1 so we can take v = Now we just need to compute the real and imaginary parts of 3i − 2 e3it cos(3t) + i sin(3t) veλ1t = e−t = e−t : (3i − 2)e3it −2 cos(3t) − 3 sin(3t) + i(3 cos(3t) − 2 sin(3t)) The general solution is thus expressed as cos(3t) sin(3t) c e−t + c e−t : 1 −2 cos(3t) − 3 sin(3t) 2 (3 cos(3t) − 2 sin(3t)) dx (b) We can examine the direction field. -
Nonlinear Multi-Mode Robust Control for Small Telescopes
NONLINEAR MULTI-MODE ROBUST CONTORL FOR SMALL TELESCOPES By WILLIAM LOUNSBURY Submitted in partial fulfillment of the requirements for the degree of Master of Science Department of Electrical Engineering and Computer Science CASE WESTERN RESERVE UNIVERSITY January, 2015 1 Case Western Reserve University School of Graduate Studies We hereby approve the thesis of William Lounsbury, candidate for the degree of Master of Science*. Committee Chair Mario Garcia-Sanz Committee Members Marc Buchner Francis Merat Date of Defense: November 12, 2014 * We also certify that written approval has been obtained for any proprietary material contained therein 2 Contents List of Figures ……………….. 3 List of Tables ……………….. 5 Nomenclature ………………..5 Acknowledgments ……………….. 6 Abstract ……………….. 7 1. Background and Literature Review ……………….. 8 2. Telescope Model and Performance Goals ……………….. 9 2.1 The Telescope Model ……………….. 9 2.2 Tracking Precision ……………….. 14 2.3 Motion Specifications ……………….. 15 2.4 Switching Stability and Bumpiness ……………….. 15 2.5 Saturation ……………….. 16 2.6 Backlash ……………….. 16 2.7 Static Friction ……………….. 17 3. Linear Robust Control ……………….. 18 3.1 Unknown Coefficients……………….. 18 3.2 QFT Controller Design ……………….. 18 4. Regional Control ……………….. 23 4.1 Bumpless Switching ……………….. 23 4.2 Two Mode Simulations ……………….. 25 5. Limit Cycle Control ……………….. 38 5.1 Limit Cycles ……………….. 38 5.2 Three Mode Control ……………….. 38 5.3 Three Mode Simulations ……………….. 51 6. Future Work ……………….. 55 6.1 Collaboration with the Pontifical Catholic University of Chile ……………….. 55 6.2 Senior Project ……………….. 56 Bibliography ……………….. 58 3 List of Figures Figure 1: TRAPPIST Photo ……………….. 9 Figure 2: Control Design – Azimuth Aggressive ……………….. 20 Figure 3: Control Design – Azimuth Moderate ……………….. 21 Figure 4: Control Design – Azimuth Aggressive ………………. -
Tight Frames and Their Symmetries
Technical Report 9 December 2003 Tight Frames and their Symmetries Richard Vale, Shayne Waldron Department of Mathematics, University of Auckland, Private Bag 92019, Auckland, New Zealand e–mail: [email protected] (http:www.math.auckland.ac.nz/˜waldron) e–mail: [email protected] ABSTRACT The aim of this paper is to investigate symmetry properties of tight frames, with a view to constructing tight frames of orthogonal polynomials in several variables which share the symmetries of the weight function, and other similar applications. This is achieved by using representation theory to give methods for constructing tight frames as orbits of groups of unitary transformations acting on a given finite-dimensional Hilbert space. Along the way, we show that a tight frame is determined by its Gram matrix and discuss how the symmetries of a tight frame are related to its Gram matrix. We also give a complete classification of those tight frames which arise as orbits of an abelian group of symmetries. Key Words: Tight frames, isometric tight frames, Gram matrix, multivariate orthogonal polynomials, symmetry groups, harmonic frames, representation theory, wavelets AMS (MOS) Subject Classifications: primary 05B20, 33C50, 20C15, 42C15, sec- ondary 52B15, 42C40 0 1. Introduction u1 u2 u3 2 The three equally spaced unit vectors u1, u2, u3 in IR provide the following redundant representation 2 3 f = f, u u , f IR2, (1.1) 3 h ji j ∀ ∈ j=1 X which is the simplest example of a tight frame. Such representations arose in the study of nonharmonic Fourier series in L2(IR) (see Duffin and Schaeffer [DS52]) and have recently been used extensively in the theory of wavelets (see, e.g., Daubechies [D92]). -
Lyapunov Stability in Control System Pdf
Lyapunov stability in control system pdf Continue This article is about the asymptomatic stability of nonlineous systems. For the stability of linear systems, see exponential stability. Part of the Series on Astrodynamics Orbital Mechanics Orbital Settings Apsis Argument Periapsy Azimut Eccentricity Tilt Middle Anomaly Orbital Nodes Semi-Large Axis True types of anomalies of two-door orbits, by the eccentricity of the Circular Orbit of the Elliptical Orbit Orbit Transmission of Orbit (Hohmann transmission of orbitBi-elliptical orbit of transmission of orbit) Parabolic orbit Hyperbolic orbit Radial Orbit Decay Orbital Equation Dynamic friction Escape speed Ke Kepler Equation Kepler Acts Planetary Motion Orbital Period Orbital Speed Surface Gravity Specific Orbital Energy Vis-viva Equation Celestial Gravitational Mechanics Sphere Influence of N-Body OrbitLagrangian Dots (Halo Orbit) Lissajous Orbits The Lapun Orbit Engineering and Efficiency Of the Pre-Flight Engineering Mass Ratio Payload ratio propellant the mass fraction of the Tsiolkovsky Missile Equation Gravity Measure help the Oberth effect of Vte Different types of stability can be discussed to address differential equations or differences in equations describing dynamic systems. The most important type is that of stability decisions near the equilibrium point. This may be what Alexander Lyapunov's theory says. Simply put, if solutions that start near the equilibrium point x e display style x_e remain close to x e display style x_ forever, then x e display style x_ e is the Lapun stable. More strongly, if x e displaystyle x_e) is a Lyapunov stable and all the solutions that start near x e display style x_ converge with x e display style x_, then x e displaystyle x_ is asymptotically stable. -
Week 8-9. Inner Product Spaces. (Revised Version) Section 3.1 Dot Product As an Inner Product
Math 2051 W2008 Margo Kondratieva Week 8-9. Inner product spaces. (revised version) Section 3.1 Dot product as an inner product. Consider a linear (vector) space V . (Let us restrict ourselves to only real spaces that is we will not deal with complex numbers and vectors.) De¯nition 1. An inner product on V is a function which assigns a real number, denoted by < ~u;~v> to every pair of vectors ~u;~v 2 V such that (1) < ~u;~v>=< ~v; ~u> for all ~u;~v 2 V ; (2) < ~u + ~v; ~w>=< ~u;~w> + < ~v; ~w> for all ~u;~v; ~w 2 V ; (3) < k~u;~v>= k < ~u;~v> for any k 2 R and ~u;~v 2 V . (4) < ~v;~v>¸ 0 for all ~v 2 V , and < ~v;~v>= 0 only for ~v = ~0. De¯nition 2. Inner product space is a vector space equipped with an inner product. Pn It is straightforward to check that the dot product introduces by ~u ¢ ~v = j=1 ujvj is an inner product. You are advised to verify all the properties listed in the de¯nition, as an exercise. The dot product is also called Euclidian inner product. De¯nition 3. Euclidian vector space is Rn equipped with Euclidian inner product < ~u;~v>= ~u¢~v. De¯nition 4. A square matrix A is called positive de¯nite if ~vT A~v> 0 for any vector ~v 6= ~0. · ¸ 2 0 Problem 1. Show that is positive de¯nite. 0 3 Solution: Take ~v = (x; y)T . Then ~vT A~v = 2x2 + 3y2 > 0 for (x; y) 6= (0; 0). -
Gram Matrix and Orthogonality in Frames 1
U.P.B. Sci. Bull., Series A, Vol. 80, Iss. 1, 2018 ISSN 1223-7027 GRAM MATRIX AND ORTHOGONALITY IN FRAMES Abolhassan FEREYDOONI1 and Elnaz OSGOOEI 2 In this paper, we aim at introducing a criterion that determines if f figi2I is a Bessel sequence, a frame or a Riesz sequence or not any of these, based on the norms and the inner products of the elements in f figi2I. In the cases of Riesz and Bessel sequences, we introduced a criterion but in the case of a frame, we did not find any answers. This criterion will be shown by K(f figi2I). Using the criterion introduced, some interesting extensions of orthogonality will be presented. Keywords: Frames, Bessel sequences, Orthonormal basis, Riesz bases, Gram matrix MSC2010: Primary 42C15, 47A05. 1. Preliminaries Frames are generalizations of orthonormal bases, but, more than orthonormal bases, they have shown their ability and stability in the representation of functions [1, 4, 10, 11]. The frames have been deeply studied from an abstract point of view. The results of such studies have been used in concrete frames such as Gabor and Wavelet frames which are very important from a practical point of view [2, 9, 5, 8]. An orthonormal set feng in a Hilbert space is characterized by a simple relation hem;eni = dm;n: In the other words, the Gram matrix is the identity matrix. Moreover, feng is an orthonor- mal basis if spanfeng = H. But, for frames the situation is more complicated; i.e., the Gram Matrix has no such a simple form. -
Uniqueness of Low-Rank Matrix Completion by Rigidity Theory
UNIQUENESS OF LOW-RANK MATRIX COMPLETION BY RIGIDITY THEORY AMIT SINGER∗ AND MIHAI CUCURINGU† Abstract. The problem of completing a low-rank matrix from a subset of its entries is often encountered in the analysis of incomplete data sets exhibiting an underlying factor model with applications in collaborative filtering, computer vision and control. Most recent work had been focused on constructing efficient algorithms for exact or approximate recovery of the missing matrix entries and proving lower bounds for the number of known entries that guarantee a successful recovery with high probability. A related problem from both the mathematical and algorithmic point of view is the distance geometry problem of realizing points in a Euclidean space from a given subset of their pairwise distances. Rigidity theory answers basic questions regarding the uniqueness of the realization satisfying a given partial set of distances. We observe that basic ideas and tools of rigidity theory can be adapted to determine uniqueness of low-rank matrix completion, where inner products play the role that distances play in rigidity theory. This observation leads to efficient randomized algorithms for testing necessary and sufficient conditions for local completion and for testing sufficient conditions for global completion. Crucial to our analysis is a new matrix, which we call the completion matrix, that serves as the analogue of the rigidity matrix. Key words. Low rank matrices, missing values, rigidity theory, iterative methods, collaborative filtering. AMS subject classifications. 05C10, 05C75, 15A48 1. Introduction. Can the missing entries of an incomplete real valued matrix be recovered? Clearly, a matrix can be completed in an infinite number of ways by replacing the missing entries with arbitrary values. -
Stability Analysis of Nonlinear Systems Using Lyapunov Theory – I
Lecture – 33 Stability Analysis of Nonlinear Systems Using Lyapunov Theory – I Dr. Radhakant Padhi Asst. Professor Dept. of Aerospace Engineering Indian Institute of Science - Bangalore Outline z Motivation z Definitions z Lyapunov Stability Theorems z Analysis of LTI System Stability z Instability Theorem z Examples ADVANCED CONTROL SYSTEM DESIGN 2 Dr. Radhakant Padhi, AE Dept., IISc-Bangalore References z H. J. Marquez: Nonlinear Control Systems Analysis and Design, Wiley, 2003. z J-J. E. Slotine and W. Li: Applied Nonlinear Control, Prentice Hall, 1991. z H. K. Khalil: Nonlinear Systems, Prentice Hall, 1996. ADVANCED CONTROL SYSTEM DESIGN 3 Dr. Radhakant Padhi, AE Dept., IISc-Bangalore Techniques of Nonlinear Control Systems Analysis and Design z Phase plane analysis z Differential geometry (Feedback linearization) z Lyapunov theory z Intelligent techniques: Neural networks, Fuzzy logic, Genetic algorithm etc. z Describing functions z Optimization theory (variational optimization, dynamic programming etc.) ADVANCED CONTROL SYSTEM DESIGN 4 Dr. Radhakant Padhi, AE Dept., IISc-Bangalore Motivation z Eigenvalue analysis concept does not hold good for nonlinear systems. z Nonlinear systems can have multiple equilibrium points and limit cycles. z Stability behaviour of nonlinear systems need not be always global (unlike linear systems). z Need of a systematic approach that can be exploited for control design as well. ADVANCED CONTROL SYSTEM DESIGN 5 Dr. Radhakant Padhi, AE Dept., IISc-Bangalore Definitions System Dynamics XfX =→() fD:Rn (a locally Lipschitz map) D : an open and connected subset of Rn Equilibrium Point ( X e ) XfXee= ( ) = 0 ADVANCED CONTROL SYSTEM DESIGN 6 Dr. Radhakant Padhi, AE Dept., IISc-Bangalore Definitions Open Set A set A ⊂ n is open if for every pA∈ , ∃⊂ Bpr () A Connected Set z A connected set is a set which cannot be represented as the union of two or more disjoint nonempty open subsets. -
Linear Independence, the Wronskian, and Variation of Parameters
LINEAR INDEPENDENCE, THE WRONSKIAN, AND VARIATION OF PARAMETERS JAMES KEESLING In this post we determine when a set of solutions of a linear differential equation are linearly independent. We first discuss the linear space of solutions for a homogeneous differential equation. 1. Homogeneous Linear Differential Equations We start with homogeneous linear nth-order ordinary differential equations with general coefficients. The form for the nth-order type of equation is the following. dnx dn−1x (1) a (t) + a (t) + ··· + a (t)x = 0 n dtn n−1 dtn−1 0 It is straightforward to solve such an equation if the functions ai(t) are all constants. However, for general functions as above, it may not be so easy. However, we do have a principle that is useful. Because the equation is linear and homogeneous, if we have a set of solutions fx1(t); : : : ; xn(t)g, then any linear combination of the solutions is also a solution. That is (2) x(t) = C1x1(t) + C2x2(t) + ··· + Cnxn(t) is also a solution for any choice of constants fC1;C2;:::;Cng. Now if the solutions fx1(t); : : : ; xn(t)g are linearly independent, then (2) is the general solution of the differential equation. We will explain why later. What does it mean for the functions, fx1(t); : : : ; xn(t)g, to be linearly independent? The simple straightforward answer is that (3) C1x1(t) + C2x2(t) + ··· + Cnxn(t) = 0 implies that C1 = 0, C2 = 0, ::: , and Cn = 0 where the Ci's are arbitrary constants. This is the definition, but it is not so easy to determine from it just when the condition holds to show that a given set of functions, fx1(t); x2(t); : : : ; xng, is linearly independent. -
Lyapunov Stability
Appendix A Lyapunov Stability Lyapunov stability theory [1] plays a central role in systems theory and engineering. An equilibrium point is stable if all solutions starting at nearby points stay nearby; otherwise, it is unstable. It is asymptotically stable if all solutions starting at nearby points not only stay nearby, but also tend to the equilibrium point as time approaches infinity. These notions are made precise as follows. Definition A.1 Consider the autonomous system [1] x˙ = f(x), (A.1) where f : D → Rn is a locally Lipschitz map from a domain D into Rn. The equilibrium point x = 0is • Stable if, for each >0, there is δ = δ() > 0 such that x(0) <δ⇒ x(t) <, ∀t ≥ 0; • Unstable if it is not stable; • Asymptotically stable if it is stable and δ can be chosen such that x(0) <δ⇒ lim x(t) = 0. t→∞ Theorem A.1 Let x = 0 be an equilibrium point for system (A.1) and D ⊂ Rn be a domain containing x = 0. Let V : D → R be a continuously differentiable function such that V(0) = 0 and V(x)>0 in D −{0}, (A.2a) V(x)˙ ≤ 0 in D. (A.2b) Then, x = 0 is stable. Moreover, if V(x)<˙ 0 in D −{0}, (A.3) then x = 0 is asymptotically stable. H.Chen,B.Gao,Nonlinear Estimation and Control of Automotive Drivetrains, 197 DOI 10.1007/978-3-642-41572-2, © Science Press Beijing and Springer-Verlag Berlin Heidelberg 2014 198 A Lyapunov Stability A function V(x)satisfying (A.2a) is said to be positive definite. -
An Introduction to the HESSIAN
An introduction to the HESSIAN 2nd Edition Photograph of Ludwig Otto Hesse (1811-1874), circa 1860 https://upload.wikimedia.org/wikipedia/commons/6/65/Ludwig_Otto_Hesse.jpg See page for author [Public domain], via Wikimedia Commons I. As the students of the first two years of mathematical analysis well know, the Wronskian, Jacobian and Hessian are the names of three determinants and matrixes, which were invented in the nineteenth century, to make life easy to the mathematicians and to provide nightmares to the students of mathematics. II. I don’t know how the Hessian came to the mind of Ludwig Otto Hesse (1811-1874), a quiet professor father of nine children, who was born in Koenigsberg (I think that Koenigsberg gave birth to a disproportionate 1 number of famous men). It is possible that he was studying the problem of finding maxima, minima and other anomalous points on a bi-dimensional surface. (An alternative hypothesis will be presented in section X. ) While pursuing such study, in one variable, one first looks for the points where the first derivative is zero (if it exists at all), and then examines the second derivative at each of those points, to find out its “quality”, whether it is a maximum, a minimum, or an inflection point. The variety of anomalies on a bi-dimensional surface is larger than for a one dimensional line, and one needs to employ more powerful mathematical instruments. Still, also in two dimensions one starts by looking for points where the two first partial derivatives, with respect to x and with respect to y respectively, exist and are both zero. -
Boundary Control of Pdes
Boundary Control of PDEs: ACourseonBacksteppingDesigns class slides Miroslav Krstic Introduction Fluid flows in aerodynamics and propulsion applications; • plasmas in lasers, fusion reactors, and hypersonic vehicles; liquid metals in cooling systems for tokamaks and computers, as well as in welding and metal casting processes; acoustic waves, water waves in irrigation systems... Flexible structures in civil engineering, aircraft wings and helicopter rotors,astronom- • ical telescopes, and in nanotechnology devices like the atomic force microscope... Electromagnetic waves and quantum mechanical systems... • Waves and “ripple” instabilities in thin film manufacturing and in flame dynamics... • Chemical processes in process industries and in internal combustion engines... • Unfortunately, even “toy” PDE control problems like heat andwaveequations(neitherof which is unstable) require some background in functional analysis. Courses in control of PDEs rare in engineering programs. This course: methods which are easy to understand, minimal background beyond calculus. Boundary Control Two PDE control settings: “in domain” control (actuation penetrates inside the domain of the PDE system or is • evenly distributed everywhere in the domain, likewise with sensing); “boundary” control (actuation and sensing are only through the boundary conditions). • Boundary control physically more realistic because actuation and sensing are non-intrusive (think, fluid flow where actuation is from the walls).∗ ∗“Body force” actuation of electromagnetic type is also possible but it has low control authority and its spatial distribution typically has a pattern that favors the near-wall region. Boundary control harder problem, because the “input operator” (the analog of the B matrix in the LTI finite dimensional model x˙ = Ax+Bu)andtheoutputoperator(theanalogofthe C matrix in y = Cx)areunboundedoperators.