Advanced Methods in Nonlinear Control Lecture Notes
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Basic Nonlinear Control Systems - D
CONTROL SYSTEMS, ROBOTICS, AND AUTOMATION – Vol. III – Basic Nonlinear Control Systems - D. P. Atherton BASIC NONLINEAR CONTROL SYSTEMS D. P. Atherton University of Sussex, UK Keywords: Nonlinearity, friction, saturation, relay, backlash, frequency response, describing function, limit cycle, stability, phase plane, subharmonics, chaos, synchronization, compensation. Contents 1. Introduction 2. Forms of nonlinearity 3. Structure and behavior 4. Stability 5. Aspects of design 6. Conclusions Glossary Bibliography Biographical Sketch Summary This section is written to introduce the reader to nonlinearity and its effect in control systems, and also to ‘set the stage’ for the subsequent articles. Nonlinearity is first defined and then some of the physical effects which cause nonlinear behavior are discussed. This is followed by some comments on the stability of nonlinear systems, the existence of limit cycles, and the unique behavioral aspects which nonlinear feedback systems may possess. Finally a few brief comments are made on designing controllers for nonlinear systems. 1. Introduction Linear systems have the important property that they satisfy the superposition principle. This leads to many important advantages in methods for their analysis. For example, in circuit theory when an RLC circuit has both d.c and a.c input voltages, the voltage or current elsewhereUNESCO in the circuit can be– found EOLSS by summing the results of separate analyses for the d.c. and a.c. inputs taken individually, also if the magnitude of the a.c. voltage is doubledSAMPLE then the a.c. voltages or CHAPTERScurrents elsewhere in the circuit will be doubled. Thus, mathematically a linear system with input x()t and output yt() satisfies the property that the output for an input ax12() t+ bx () t is ay12() t+ by () t , if y1()t and y2 ()t are the outputs in response to the inputs x1()t and x2 ()t , respectively, and a and b are constants. -
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 ………………. -
Neural Control for Nonlinear Dynamic Systems
Neural Control for Nonlinear Dynamic Systems Ssu-Hsin Yu Anuradha M. Annaswamy Department of Mechanical Engineering Department of Mechanical Engineering Massachusetts Institute of Technology Massachusetts Institute of Technology Cambridge, MA 02139 Cambridge, MA 02139 Email: [email protected] Email: [email protected] Abstract A neural network based approach is presented for controlling two distinct types of nonlinear systems. The first corresponds to nonlinear systems with parametric uncertainties where the parameters occur nonlinearly. The second corresponds to systems for which stabilizing control struc tures cannot be determined. The proposed neural controllers are shown to result in closed-loop system stability under certain conditions. 1 INTRODUCTION The problem that we address here is the control of general nonlinear dynamic systems in the presence of uncertainties. Suppose the nonlinear dynamic system is described as x= f(x , u , 0) , y = h(x, u, 0) where u denotes an external input, y is the output, x is the state, and 0 is the parameter which represents constant quantities in the system. The control objectives are to stabilize the system in the presence of disturbances and to ensure that reference trajectories can be tracked accurately, with minimum delay. While uncertainties can be classified in many different ways, we focus here on two scenarios. One occurs because the changes in the environment and operating conditions introduce uncertainties in the system parameter O. As a result, control objectives such as regulation and tracking, which may be realizable using a continuous function u = J'(x, 0) cannot be achieved since o is unknown. Another class of problems arises due to the complexity of the nonlinear function f. -
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. -
Control Theory
Control theory S. Simrock DESY, Hamburg, Germany Abstract In engineering and mathematics, control theory deals with the behaviour of dynamical systems. The desired output of a system is called the reference. When one or more output variables of a system need to follow a certain ref- erence over time, a controller manipulates the inputs to a system to obtain the desired effect on the output of the system. Rapid advances in digital system technology have radically altered the control design options. It has become routinely practicable to design very complicated digital controllers and to carry out the extensive calculations required for their design. These advances in im- plementation and design capability can be obtained at low cost because of the widespread availability of inexpensive and powerful digital processing plat- forms and high-speed analog IO devices. 1 Introduction The emphasis of this tutorial on control theory is on the design of digital controls to achieve good dy- namic response and small errors while using signals that are sampled in time and quantized in amplitude. Both transform (classical control) and state-space (modern control) methods are described and applied to illustrative examples. The transform methods emphasized are the root-locus method of Evans and fre- quency response. The state-space methods developed are the technique of pole assignment augmented by an estimator (observer) and optimal quadratic-loss control. The optimal control problems use the steady-state constant gain solution. Other topics covered are system identification and non-linear control. System identification is a general term to describe mathematical tools and algorithms that build dynamical models from measured data. -
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. -
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. -
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. -
Integral Characterizations of Asymptotic Stability
Integral characterizations of asymptotic stability ? Elena Panteleyy, Antonio Lor´ıa• and Andrew R. Teel yINRIA Rhoneˆ Alpes ZIRST - 655 Av. de l’Europe 38330 Montbonnot Saint-Martin, France [email protected] •C.N.R.S. UMR 5528 LAG-ENSIEG, B.P. 46, 38402, St. Martin d’Heres, France [email protected] ?Center for Control Engineering and Computation (CCEC) Department of Electrical and Computer Engineering University of California Santa Barbara, CA 93106-9560, USA [email protected] Keywords: UGAS, stability of sets, Lyapunov stability ever this is too restrictive. For time-varying systems, Naren- analysis. dra and Anaswamy [4] proposed to use an observability type condition which is formulated as an integral condition on the derivative of the Lyapunov function. This approach was fur- ther developed in the papers of Aeyels and Peuteman [1], Abstract where a “difference” stability criterion was formulated as a condition on the decrease of the difference between the val- We present an integral characterization of uniform global ues of the “Lyapunov” function at two time instances; more asymptotic stability (UGAS) of sets and use this character- precisely it is required that that there exists T > 0 such that ization to provide a result on UGAS of sets for systems with for all t t the following inequality is satisfied: output injection. ≥ ◦ V (t + T; x(t + T )) V (t; x) γ( x(t) ); − ≤ j j 1 Introduction where γ . The advantage2 K1 of this formulation is firstly, that the func- Starting with the original paper by Lyapunov [3], the concept tion V (t; x) is not required to be continuously differentiable of stability of solutions of a differential equation x˙ = f(t; x) nor locally Lipschitz and secondly, this formulation allows a was formulated as a stability problem with respect to some certain increase of the derivative of the Lyapunov function at function F (x) of the state. -
Applications of the Wronskian and Gram Matrices of {Fie”K?
View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by Elsevier - Publisher Connector Applications of the Wronskian and Gram Matrices of {fie”k? Robert E. Hartwig Mathematics Department North Carolina State University Raleigh, North Carolina 27650 Submitted by S. Barn&t ABSTRACT A review is made of some of the fundamental properties of the sequence of functions {t’b’}, k=l,..., s, i=O ,..., m,_,, with distinct X,. In particular it is shown how the Wronskian and Gram matrices of this sequence of functions appear naturally in such fields as spectral matrix theory, controllability, and Lyapunov stability theory. 1. INTRODUCTION Let #(A) = II;,,< A-hk)“‘k be a complex polynomial with distinct roots x 1,.. ., A,, and let m=ml+ . +m,. It is well known [9] that the functions {tieXk’}, k=l,..., s, i=O,l,..., mkpl, form a fundamental (i.e., linearly inde- pendent) solution set to the differential equation m)Y(t)=O> (1) where D = $(.). It is the purpose of this review to illustrate some of the important properties of this independent solution set. In particular we shall show that both the Wronskian matrix and the Gram matrix play a dominant role in certain applications of matrix theory, such as spectral theory, controllability, and the Lyapunov stability theory. Few of the results in this paper are new; however, the proofs we give are novel and shed some new light on how the various concepts are interrelated, and on why certain results work the way they do. LINEAR ALGEBRA ANDITSAPPLlCATIONS43:229-241(1982) 229 C Elsevier Science Publishing Co., Inc., 1982 52 Vanderbilt Ave., New York, NY 10017 0024.3795/82/020229 + 13$02.50 230 ROBERT E. -
Fundamentals of Backstepping Control
Appendix Fundamentals of Backstepping Control This Appendix provides the fundamentals of the recursive backstepping control method. The presented material is a summary of more detailed descriptions that may be found in [43, 49]. Lyapunov-based controller design may be systematically tack- led by a recursive design procedure called backstepping. Backstepping is suitable for strict-feedback systems that are also known as “lower triangular”. An example of a strict-feedback systems is: ˙ ξ1 = f1(ξ1) + g1(ξ1)ξ2 ˙ ξ2 = f2(ξ1,ξ2) + g2(ξ1,ξ2)ξ3 . (A.1) ˙ ξr−1 = fr−1(ξ1,ξ2,...,ξr−1) + gr−1(ξ1,ξ2,...,ξr−1)ξr ˙ ξr = fr (ξ1,ξ2,...,ξr ) + gr (ξ1,ξ2,...,ξr )u where ξ1,...,ξr ∈ R, u ∈ R is the control input and fi , gi for i = 1,...,r are known functions. A typical feedback linearization approach in most cases leads to cancellation of useful nonlinearities. The backstepping design exhibits more flexi- bility compared to feedback linearization since it does not require that the resulting input–output dynamics be linear. Cancellation of potentially useful nonlinearities can be avoided resulting in less complex controllers. The main idea is to use some of the state variables of (A.1) as “virtual controls” or “pseudo controls”, and de- pending on the dynamics of each state, design intermediate control laws. The back- stepping design is a recursive procedure where a Lyapunov function is derived for the entire system. The recursive procedure can be easily expanded from the nominal case of a system augmented by an integrator. This is also referred to as integra- tor backstepping.