Ordinary Differential Equation
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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 ………………. -
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. -
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. -
18.700 JORDAN NORMAL FORM NOTES These Are Some Supplementary Notes on How to Find the Jordan Normal Form of a Small Matrix. Firs
18.700 JORDAN NORMAL FORM NOTES These are some supplementary notes on how to find the Jordan normal form of a small matrix. First we recall some of the facts from lecture, next we give the general algorithm for finding the Jordan normal form of a linear operator, and then we will see how this works for small matrices. 1. Facts Throughout we will work over the field C of complex numbers, but if you like you may replace this with any other algebraically closed field. Suppose that V is a C-vector space of dimension n and suppose that T : V → V is a C-linear operator. Then the characteristic polynomial of T factors into a product of linear terms, and the irreducible factorization has the form m1 m2 mr cT (X) = (X − λ1) (X − λ2) ... (X − λr) , (1) for some distinct numbers λ1, . , λr ∈ C and with each mi an integer m1 ≥ 1 such that m1 + ··· + mr = n. Recall that for each eigenvalue λi, the eigenspace Eλi is the kernel of T − λiIV . We generalized this by defining for each integer k = 1, 2,... the vector subspace k k E(X−λi) = ker(T − λiIV ) . (2) It is clear that we have inclusions 2 e Eλi = EX−λi ⊂ E(X−λi) ⊂ · · · ⊂ E(X−λi) ⊂ .... (3) k k+1 Since dim(V ) = n, it cannot happen that each dim(E(X−λi) ) < dim(E(X−λi) ), for each e e +1 k = 1, . , n. Therefore there is some least integer ei ≤ n such that E(X−λi) i = E(X−λi) i . -
(VI.E) Jordan Normal Form
(VI.E) Jordan Normal Form Set V = Cn and let T : V ! V be any linear transformation, with distinct eigenvalues s1,..., sm. In the last lecture we showed that V decomposes into stable eigenspaces for T : s s V = W1 ⊕ · · · ⊕ Wm = ker (T − s1I) ⊕ · · · ⊕ ker (T − smI). Let B = fB1,..., Bmg be a basis for V subordinate to this direct sum and set B = [T j ] , so that k Wk Bk [T]B = diagfB1,..., Bmg. Each Bk has only sk as eigenvalue. In the event that A = [T]eˆ is s diagonalizable, or equivalently ker (T − skI) = ker(T − skI) for all k , B is an eigenbasis and [T]B is a diagonal matrix diagf s1,..., s1 ;...; sm,..., sm g. | {z } | {z } d1=dim W1 dm=dim Wm Otherwise we must perform further surgery on the Bk ’s separately, in order to transform the blocks Bk (and so the entire matrix for T ) into the “simplest possible” form. The attentive reader will have noticed above that I have written T − skI in place of skI − T . This is a strategic move: when deal- ing with characteristic polynomials it is far more convenient to write det(lI − A) to produce a monic polynomial. On the other hand, as you’ll see now, it is better to work on the individual Wk with the nilpotent transformation T j − s I =: N . Wk k k Decomposition of the Stable Eigenspaces (Take 1). Let’s briefly omit subscripts and consider T : W ! W with one eigenvalue s , dim W = d , B a basis for W and [T]B = B. -
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. -
System Stability
7 System Stability During the description of phase portrait construction in the preceding chapter, we made note of a trajectory’s tendency to either approach the origin or diverge from it. As one might expect, this behavior is related to the stability properties of the system. However, phase portraits do not account for the effects of applied inputs; only for initial conditions. Furthermore, we have not clarified the definition of stability of systems such as the one in Equation (6.21) (Figure 6.12), which neither approaches nor departs from the origin. All of these distinctions in system behavior must be categorized with a study of stability theory. In this chapter, we will present definitions for different kinds of stability that are useful in different situations and for different purposes. We will then develop stability testing methods so that one can determine the characteristics of systems without having to actually generate explicit solutions for them. 7.1 Lyapunov Stability The first “type” of stability we consider is the one most directly illustrated by the phase portraits we have been discussing. It can be thought of as a stability classification that depends solely on a system’s initial conditions and not on its input. It is named for Russian scientist A. M. Lyapunov, who contributed much of the pioneering work in stability theory at the end of the nineteenth century. So- called “Lyapunov stability” actually describes the properties of a particular point in the state space, known as the equilibrium point, rather than referring to the properties of the system as a whole. -
Your PRINTED Name Is: Please Circle Your Recitation
18.06 Professor Edelman Quiz 3 December 3, 2012 Grading 1 Your PRINTED name is: 2 3 4 Please circle your recitation: 1 T 9 2-132 Andrey Grinshpun 2-349 3-7578 agrinshp 2 T 10 2-132 Rosalie Belanger-Rioux 2-331 3-5029 robr 3 T 10 2-146 Andrey Grinshpun 2-349 3-7578 agrinshp 4 T 11 2-132 Rosalie Belanger-Rioux 2-331 3-5029 robr 5 T 12 2-132 Georoy Horel 2-490 3-4094 ghorel 6 T 1 2-132 Tiankai Liu 2-491 3-4091 tiankai 7 T 2 2-132 Tiankai Liu 2-491 3-4091 tiankai 1 (16 pts.) a) (4 pts.) Suppose C is n × n and positive denite. If A is n × m and M = AT CA is not positive denite, nd the smallest eigenvalue of M: (Explain briey.) Solution. The smallest eigenvalue of M is 0. The problem only asks for brief explanations, but to help students understand the material better, I will give lengthy ones. First of all, note that M T = AT CT A = AT CA = M, so M is symmetric. That implies that all the eigenvalues of M are real. (Otherwise, the question wouldn't even make sense; what would the smallest of a set of complex numbers mean?) Since we are assuming that M is not positive denite, at least one of its eigenvalues must be nonpositive. So, to solve the problem, we just have to explain why M cannot have any negative eigenvalues. The explanation is that M is positive semidenite.