Book

Nonlinear Control Systems II

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Abstract

From the Publisher: "This book incorporates recent advances in the design of feedback laws to the purpose of globally stabilizing nonlinear systems via state or output feedback. It is a continuation of the first volume by Alberto Isidori on Nonlinear Control Systems. Specifically this second volume will cover: Stability analysis of interconnected nonlinear systems; the notion of input-to-state stability and its role in analysing stability of cascade-connected or feedback-connected systems; the notion of dissipativity and its consequences (passivity and "gain"); robust stabilization in the case of parametric uncertainties; the case of state feedback (global or semi-global stabilization); the case of output feedback (semi-global stabilization); robust stabilization in the case of unstructured perturbations; feedback design via the small-gain approach; robust semi-global stabilization via output feedback; methods for asymptotic tracking, disturbance rejection and model following; global and semi-global analysis; normal forms for multi-input multi-output nonlinear systems form a global point of view; and their role in feedback design."--BOOK JACKET.

Chapters (5)

For convenience of the reader, this section provides a quick review of the notion of comparison functions and their role in the well-known criterion of Lyapunov for determining stability and asymptotic stability.
The purpose of this Chapter is to describe some important tools for the design of feedback laws which globally asymptotically stabilize a nonlinear system in the presence of parameter uncertainties. We consider the case in which the mathematical model of the system to be controlled depends on a vector μ ∈ ℝp of parameters, which are assumed to be constant, but whose actual values are unknown to the designer. The vector µ of unknown parameters could be any vector in some a priori given set \( \mathcal{P} \), and the goal of the design is to find a feedback law (obviously independent of μ) which globally asymptotically stabilizes the system for each value of \( \mu \in \mathcal{P} \). A problem of this type is usually referred to as a problem of robust stabilization.
In section 9.3 we have introduced the concept of semiglobal stabilizability, and we have shown (Theorem 9.3.1) how, using a linear feedback, it is possible to stabilize in a semiglobal sense (i.e. imposing that the domain of attraction of the equilibrium contains a prescribed compact set) a system of the form (9.23), under the hypothesis that the equilibrium z = 0 of its zero dynamics is globally asymptotically stable. In this section, in preparation to the subsequent study of the problem of robust semiglobal stabilization using output feedback, we extend the result of Theorem 9.3.1 to the case of a system modeled by equations of the form $$\begin{array}{*{20}{l}} {\dot z}& = &{{f_0}(z,\xi )} \\ {{{\dot \xi }_1}}& = &{{\xi _2}} \\ {{{\dot \xi }_2}}& = &{{\xi _3}} \\ {}&{}& \cdots \\ {{{\dot \xi }_r}}& = &{q(z,{\xi _1}, \ldots ,{\xi _r},\mu ) + b(z,{\xi _1}, \ldots ,{\xi _r},\mu )u,} \end{array}$$ (1) in which z ∈ ℝn , ξi ∈ ℝ for i=1,…,r, u ∈ ℝ and \(\mu \in \mathcal{P} \subset {\mathbb{R}^p}\) is a vector of unknown parameters, ranging over a compact set \(\mathcal{P}\).
In this Chapter we will study problems of global stabilization of systems that can be modeled as feedback interconnection of two subsystems, one of which is accurately known while the other one is uncertain but has a finite L 2 gain, for which an upper bound is available. More precisely, we consider systems modeled by equations of the form $$\begin{array}{*{20}{l}} {{{\dot x}_1}}& = &{{f_1}({x_1},{h_2}({x_2}),u)} \\ {{{\dot x}_2}}& = &{{f_2}({x_2},{h_1}({x_1})),} \end{array}$$ (13.1) which describe the feedback interconnection of a system $$\begin{array}{*{20}{l}} {{{\dot x}_1}}& = &{{f_1}({x_1},w,u)} \\ y& = &{{h_1}({x_1})} \end{array}$$ (13.2) in which \({x_1} \in {\mathbb{R}^{{n_1}}}\), w ∈ ℝ, u ∈ ℝ, y ∈ ℝ and f 1(0,0,0)=0, h 1(0)=0, a system $$\begin{array}{*{20}{l}} {{{\dot x}_2}}& = &{{f_2}({x_2},y)} \\ w& = &{{h_2}({x_2})} \end{array}$$ (13.3) in which \({x_2} \in {\mathbb{R}^{{n_2}}}\) and f 2(0,0)=0,h 2(0)=0.
In this Chapter, we describe methods for global (robust) stabilization of nonlinear systems, by means of memoryless feedback, in cases in which the amplitude of the control input cannot exceed a fixed bound. Of course, if such a hard constraint is imposed on the amplitude of the control input, one cannot expect — in general — that global asymptotic stability is possible, unless the uncontrolled system already possesses this property to a certain extent. The simplest case in which so happens is when there exists a positive definite and proper function, whose derivative along the trajectories of the uncontrolled system is negative semi-definite but, possibly, not negative definite. In this case, in fact, under mild hypotheses, it is possible to find a smooth feedback law, whose amplitude does not exceed any (arbitrarily small) a priori fixed number, yielding global asymptotic stability. We discuss this special case first, as a point of departure for the analysis of more general structures that will be presented in the subsequent sections of the Chapter.
... where the known boundsd 0 , d n1 and d n2 can be retrieved for instance from the physical characteristics of the plant. Taking into account the foregoing problem formulation, the control objective is to design the control laws u 0 and u 1 appearing in (1) such that [x 0 , x ⊤ ] ⊤ , as t → ∞, converges to a small vicinity of the equilibrium point, which will be formally defined in the sequel of the paper relying on the concept of Input-to-State Stability [35], and all the other signals in the closed-loop system are bounded. Note that the triangular structure of system (1) allows us to design the control inputs u 0 and u 1 in two separate steps. ...
... with k j > 0, substituting in (35), exploiting (31) and posinĝ ∆ j =ŵ ⊤ j b j , one haṡ ...
... Then, by relying on the concept of Input-to-State-Stability (ISS) [35], the following result can be proved. ...
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... Los campos vectoriales f (t, z) y g (t, z) en R n son suaves e inciertos, y la dimensión n puede ser también incierta. Un problema básico de control consiste en la estabilización robusta del origen z = 0 de (1), a pesar de las incertidumbres y/o perturbaciones presentes en f y g (Khalil, 2002;Isidori, 1995Isidori, , 1999. Nótese que problemas de seguimiento robusto de referencias variantes en el tiempo pueden ser reformulados como problemas de estabilización robusta. ...
... Los campos vectoriales f (t, z) y g (t, z) en R n son suaves e inciertos, y la dimensión n puede ser también incierta. Un problema básico de control consiste en la estabilización robusta del origen z = 0 de (1), a pesar de las incertidumbres y/o perturbaciones presentes en f y g (Khalil, 2002;Isidori, 1995Isidori, , 1999. Nótese que problemas de seguimiento robusto de referencias variantes en el tiempo pueden ser reformulados como problemas de estabilización robusta. ...
... dónde σ ∈ R y h : R × R n → R es una función suave. σ debe ser tal que: a) σ tenga grado relativo ρ ≥ 1 bien definido (Isidori, 1995) con respecto a u, es decir, ...
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En este trabajo se presenta una panorámica del desarrollo de los métodos básicos de análisis y diseño de controladores y observadores por modos deslizantes de orden superior. Inicialmente se describen los controladores por retroalimentación de estados con una ley de control discontinua, que generan un modo deslizante de cualquier orden. Posteriormente se presenta una nueva clase de algoritmos por modos deslizantes de orden superior, que consisten en una retroalimentación de estados continua y una acción de control integral discontinua. Se describen también observadores por modos deslizantes, que estiman los estados del sistema en tiempo finito, y que permiten obtener un controlador por retroalimentación de la salida. Todos los diseños presentados se basan en el uso de funciones de Lyapunov (explícitas), que constituyen una contribución importante del grupo de trabajo de los autores en la Universidad Nacional Autónoma de México. La presentación es tutorial y solo se dan los resultados, dejando a un lado la formalización rigurosa y las pruebas matemáticas. Para ello se refiere al lector a la literatura pertinente. Se ilustran los resultados mediante simulaciones y la validación experimental en un sistema de levitación magnética.
... In the linear case this inequality reduces to a more tractable matrix algebraic Riccati inequality. Furthermore, the powerful concept of Input-to-State Stability (ISS) is strongly related to L ∞ −stability, and constitutes an important generalization [2], [6], [8]- [10]. ...
... Apparently, it is important to understand the concepts of L p −stability and L p −gain for homogeneous systems. Since, in general, homogeneous systems may be non-smooth and their linearizations (when meaningful) are trivial, many of the standard results for non-linear systems [2], [6]- [8] cannot be used. ...
... An inequality of the type of (22) with p = q = 2 is classically used to charaterize the L 2 −gain of a non-linear system [2], [6]- [8]. In the linear case this reduces to the well-known Riccati inequality, when choosing a quadratic V (x). ...
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The motivation of this paper comes from the fact that $\mathcal {L}_{p}-$ stability and $\mathcal {L}_{p}-$ gain, using the classical signal norms, is not well-defined for arbitrary continuous weighted homogeneous systems. However, using homogeneous signal norms it is possible to show that every internally stable homogeneous system has a globally defined finite homogeneous $\mathcal {L}_{p}-$ gain, for $p$ sufficiently large. If the system has a homogeneous approximation, the homogeneous $\mathcal {L}_{p}-$ gain is inherited locally. Homogeneous $\mathcal {L}_{p}-$ stability can be characterized by a homogeneous dissipation inequality, which in the input affine case can be transformed to a homogeneous Hamilton-Jacobi inequality. An estimation of an upper bound for the homogeneous $\mathcal {L}_{p}-$ gain can be derived from these inequalities. Homogeneous $\mathcal {L}_{\infty }-$ stability is also considered and its strong relationship to Input-to-State stability is studied. These results are extensions to arbitrary homogeneous systems of the well-known situation for linear time-invariant systems, where the Hamilton-Jacobi inequality reduces to an algebraic Riccati inequality. A natural application of finite-gain homogeneous $\mathcal {L}_{p}-$ stability is in the study of stability for interconnected systems. An extension of the small-gain theorem for negative feedback systems and results for systems in cascade are derived for different homogeneous norms. Previous results in the literature use classical signal norms, hence, they can only be applied to a restricted class of homogeneous systems. The results are illustrated by several examples.
... Hence, nonlinear systems are typical research models in various control fields and can be used to describe the dynamics of the system states. In order to handle nonlinear control problems, many classical control methods were proposed based on the nonlinear control theory [1][2][3], such as the baskstepping control method, feedback linearization technique, and nonlinear disturbance observer-based control scheme. Based on these nonlinear control theories, a number of advanced control techniques were proposed for various control systems. ...
... A. The Calculation of d((k 5 + H 25 + (H 24 /4‖u 1 ‖ (4/3)) + (3ε 25 /4‖u 1 ...
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In this paper, an antidisturbance controller is presented for helicopter stochastic systems under disturbances. To enhance the antidisturbance abilities, the nonlinear disturbance observer method is applied to reject the time-varying disturbances. Then, the antidisturbance nonlinear controller is designed by combining the backstepping control scheme. And the stochastic theory is used to guarantee that the closed-loop system is asymptotically bounded in mean square while the proposed control method is shown via some traditional nonlinear control techniques, which still show some common issues such as “dimension explosion” or others. The result of this paper can be regarded as a typical case of the nonlinear control method to help and promote the generation of advanced methods.
... However, even though ML researchers have provided some theoretical guarantees (Sutton and Barto, 1998), this rests in contrast to the CT paradigm, where provable guarantees are a design specification (e.g., see feedback linearization (Isidori, 1999) for convergence and prescribed performance control (Bechlioulis and Rovithakis, 2008) for output constraints). For example, in the context of the motion planning problem, there exist a variety of conventional algorithms that provide provable guarantees, whereas ML approachesmostly aim at achieving a desired control performance, without imposing the latter by design, hence, a statistical analysis may be applied to asses the effectiveness of the method. ...
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... with x ∈ R nx , u ∈ R and f, g to be sufficiently smooth of suitable dimension. Let q : R nx → R be a C 1 function and let r ∈ N. We say that the function y = q(x) has a relative degree 1 r with respect to system (8) and input u in the sense of [9,Section 4] ...
... Combining the Equations (26), (28), and (29), the extended system state space model of ADRC and controlled system is established. ...
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... Fortunately, for the 3D overhead crane with 6-Dof, all dependent states are weakly stable when the control-directly states are stable at the equibrilium points. This property suggests a method to design a feedback controller to make the system to be stable and it is also satisfying Alberto Isidori's sufficient condition for the stability of the underactuated system studied in [9]. ...
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This paper proposes a novel scheme for stabilization of the 6-DoF Overhead Crane to control the movements of this system without the state measurements through the separation principle. The movements of the system studied in this paper are described more closely than the existing crane model when considering six behaviors simultaneously: the movement of the trolley and the bridge, two swing angles along the x-axis and y-axis of the payload, the hoisting drum rotation, and axial payload oscillation. The mission of the proposal is to make all the above behaviors of the 6-DOF crane system to be stable accurately enough at the desired positions and minimize both the horizontal swings of the payload and the axial oscillation of the cable by utilizing information about the position of the trolley, the bridge, and the length of cable. To guarantee these objectives, a cooperation regime controller comprising a new asymptotic state observer which is elaborately constructed via a neural network, and the output feedback backstepping hierarchical sliding mode vehicle is integrated into the controller for improving the adaption of the closed-loop system. This cooperation controller is also evolved to prop up the fault injection data onslaught by eliminating all the information about the input system into the procedure. Furthermore, to enhance the flexibility of the closed scheme, an updating law for the observer’s parameter is developed based on the data-driven principle. All of them are developed and designed not only to handle these above tasks but also to avoid the undesired finite-escape-time (FET) phenomenon. All the results are proven systematically by three theorems and validated their performance through two scenarios and simulated by Matlab/Simulink platform.
... For this purpose, consider a system which, in addition to the control input u, is also influenced by a disturbance w. In the case with affinity to the input, the system can be described as followṡ (56) by the vector fields f , g 1 , g 2 : R n → R n . Definition 1 can be generalized as follows [7,66,67]: ...
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This paper deals with systematic approaches for the analysis of stability properties and controller design for nonlinear dynamical systems. Numerical methods based on sum-of-squares decomposition or algebraic methods based on quantifier elimination are used. Starting from Lyapunov’s direct method, these methods can be used to derive conditions for the automatic verification of Lyapunov functions as well as for the structural determination of control laws. This contribution describes methods for the automatic verification of (control) Lyapunov functions as well as for the constructive determination of control laws.
... Nonlinear control systems are widely used in aerospace, robotics, power systems, and mechatronics fields. [12,13]. ...
... Upon (13), one observes that in the conventional ADRC system the tracking error dynamics and a terminal upper bound of error (4) are forced by the aggregated estimation deviation ∆(t). The residual deviation lim sup t→∞ |∆(t)|, and as a consequence of (13) -by the Input-to-State-Stability result, [10] -also lim sup →∞ |e(t)|, can be made sufficiently small (at least in the perfect measurement conditions) by increasing the bandwidth of LESO, that is, by increasing the parameter ω o , see [15]. This well known high-gain observation strategy has substantial practical limitation due to the possible presence of a high-frequency measurement noise z corrupting the output signal y. ...
... . The stability analysis of cascaded systems has been thoroughly explored, see for example Isidori (1999); Sepulchre et al. (1997), and two main methods exist to infer the asymptotic stability of the cascaded system. These methods rely on satisfying either: ...
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Chapter
The purpose of this chapter is to review some notions of fundamental importance on the analysis and design of feedback laws for nonlinear control systems. The first part of the chapter begins by reviewing the notion of dynamical system and continues with a discussion of the concepts of stability and asymptotic stability of an equilibrium, with emphasis on the method of Lyapunov. Then, it continues by reviewing the notion of input-to-state stability and discussing its role in the analysis of interconnections of systems. Then, the first part is concluded by the analysis of the asymptotic behavior in the presence of persistent inputs. The second part of the chapter is devoted to the presentation of systematic methods for stabilization of relevant classes of nonlinear systems, namely, those possessing a globally defined normal form. Methods for the design of full-state feedback and, also, observer-based dynamic output feedback are presented. A nonlinear separation principle, based on the use of a high-gain observer, is discussed. A special role, in this context, is played by the methods based on feedback linearization, of which a robust version, based on the use of extended high-gain observer, is also presented.KeywordsDynamical systemsStabilityMethod of LyapunovInput-to-state stabilitySteady-state behaviorNormal formsFeedback linearizationBacksteppingHigh-gain observersSeparation principleExtended observers
Conference Paper
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Chapter
Motion control methods of manipulators with flexible-joint or flexible-link are different from rigid manipulators due to different composition and characteristics Yan et al. (IEEE Trans. Syst., Man, Cybern.: Syst. 51(3):1671–1678, 2021), Reis and da Costa (J. Sound Vib. 331(14):3255–3270, 2012).
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Chapter
An objective of a control theory is to influence the dynamics of a system to guarantee its desired behavior. Challenges arising in this way are manifold and include nonlinearity of a system, a need to ensure robustness (or reliability) of designed controllers in spite of actuator and observation errors, hidden (unmodeled) dynamics of a system, and external disturbances acting on the system. Furthermore, networks to be controlled may be huge with a nontrivial topological structure.
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