The objective of adaptive control is to design a controller that can adjust its behaviour to tolerate uncertain or time-varying parameters. An adaptive controller typically consists of a linear time-invariant (LTI) compensator together with a tuning mechanism which adjusts the compensator parameters and yields a nonlinear controller. Because of the nonlinearity, the transient closed-loop behaviour is often poor and the control signal may become unduly large. Although the initial objective of adaptive control was to deal with time-varying plant parameters, most classical adaptive controllers cannot handle rapidly changing parameters. Recently, the use of a linear periodic (LP) controller has been proposed as a new approach in the field of model reference adaptive control [1]. In this new approach, instead of estimating plant parameters, the “ideal control signal” (what the control signal would be if the plant parameters and states were measurable) is estimated. The resulting controller has a number of desirable features: (1) it handles rapid changes in the plant parameters, (2) it provides nice transient behaviour of the closed-loop system, (3) it guarantees that the effect of the initial conditions declines to zero exponentially, and (4) it generates control signals which are modest in size. Although the linear periodic controller (LPC) has the above advantages, it has some imperfections. In order to achieve the desirable features, a rapidly varying control signal and a small sampling period are used. The rapidly time-varying control signal requires fast actuators which may not be practical. The second weakness of the LPC [1] is poor noise rejection behaviour. The small sampling period results in large controller gains and correspondingly poor noise sensitivity, since there is a clear trade-off between tracking and noise tolerance. As the last drawback, this controller requires knowledge of the exact plant relative degree. Here we extend this work in several directions: (i) In [1], the infinity-norm is used to measure the signal size. Here we redesign the controller to yield a new version which provides comparable results when the more common 2-norm is used to measure signal size, (ii) A key drawback of the controller of [1] is that the control signal moves rapidly. Here we redesign the control law to significantly alleviate this problem, (iii) The redesigned controller can handle large parameter variation and in the case that the sign of high frequency gain is known, the closed-loop system is remarkably noise-tolerant, (iv) We prove that in an important special case, we can replace the requirement of knowledge of the exact relative degree with that of an upper bound on the relative degree, at least from the point of view of providing stability, and (v) A number of approaches to improve the noise behaviour of the controller are presented. Reference: [1] D. E. Miller, “A New Approach to Model Reference Adaptive Control”, IEEE Transaction on Automatic Control, Vol. 48, No. 5, pages 743-756, May 2003.

<p>This thesis is divided in to two different parts. The first part includes examination of the measurementsystem of an industrial robot using a resolver sensor. The main focus is on methods for suppressing noise in the angularvelocity signal without increasing timedelay. Five different methods are investigated. Three of these are based on oversampling: burstsamplingmethod, meanvaluemethod and correlationmethod. The meanvaluemethod and the correlationmethod have given good results. The two other methods are: extended kalmanfiltering and computation of the angular velocity without using numeric method to compute the angle. Extended kalmanfilter gives the overall best result. </p><p>In part two the control structure design of an industrial robot has been studied and how different sampling times and motorinertias affect the disturbance rejection and stability of the control loop. Different control structure designs have also been studied with the aim to suppress disturbances. Mainly H-infinity and GIMC designs have been compared with an ordinary PID controller. Here it can be shown that both the H-infinity and the GIMC controller yields good disturbance rejection. But both the methods lack in the robustness of model uncertainty.</p>

This paper presents the development of building up a controlled MEMS acceleration sensor. The first samples have archived a resolution of better than 500 ug and a bandwidth of more than 200 Hz. A theoretical model is built from the physical principles of the complete sensor system, consisting of the MEMS sensor, the charge amplifier and the PWM driver for the sensor element. A reduced order model of the system is used to design a robust control with the Mixed-Sensitivity H-infinity Approach. Limitations for the control design are given since the system contains time delays and an unstable pole imposed by the electrostatic spring softening effect. The theoretical model might be inaccurate or lacks of completeness, because the parameters for the theoretical model building vary from sample to sample or might be not known. A new two-stage identification scheme is deployed to obtain directly the system parameters from the samples. The focus of this paper is the complete system development and identification process including practical tests in a DSP TI-TMS320C3000 environment with 12/14-bit A/D-D/A converters. / Der Artikel beschreibt die Entwicklungsschritte eines geregelten MEMS-Beschleunigungssensors. Die ersten Prototypen erreichten dabei eine Auflösung von weniger als 500 ug und eine Bandbreite von mehr als 200 Hz. Ein theoretisches Modell für den Reglerentwurf wird aus den physikalischen Zusammenhängen des Gesamtsystems, bestehend aus dem mechanischen Sensorelement, dem Ladungsverstärker und der PWM-Treiberstufe, gebildet. Für den Reglerentwurf wird der H-Infinity Mixed-Sensitivity Approach verwendet. Wegen Systemtotzeiten und dem Effekt der elektrostatischen Federerweichung sind Grenzen für die Wahl der Bandbreite zu beachten. Da Parameter für das theoretische Modell stark variieren oder schwer zu bestimmen sind, wird eine 2-Stufen-Identifikationsmethode vorgeschlagen, um ein Modell für den Reglerentwurf zu erhalten. Praktische Tests wurden mit einem DSP TI-TMS320C3000 mit 12/14-Bit A/D-D/A Wandlerstufen durchgeführt.

Extremely large telescopes (ELTs) are the next generation of ground-based reflecting telescopes of optical wavelengths. ELTs possess an aperture of more than 20 meters and share a number of common features, particularly the use of a segmented primary mirror and the use of adaptive optics systems. In 2005, the European Southern Observatory introduced a new giant telescope concept, named the European Extremely Large Telescope (E-ELT), which is scheduled for operation in 2018. The E-ELT will address key scientific challenges and will aim for a number of notable firsts, including discovering Earth-like planets around other stars in the ``habitable zones'' where life could exist, attempting to uncover the relationship between black holes and galaxies, measuring the properties of the first stars and galaxies, and probing the nature of dark matter and dark energy. In 2009, a feasibility study, conducted by National Instruments, proved the feasibility of the real-time (RT) control system architecture for the E-ELT's nearly 1,000 mirror segments with 3,000 actuators and 6,000 sensors. The goal of the RT control system was to maintain a perfectly aligned field of mirrors at all times with a loop-time of 1 ms. The study assumed a prescribed controller algorithm. This research report prescribes the optimal controller algorithms for large segmented telescopes. In this respect, optimal controller designs for the primary mirror of the E-ELT, where optimality is formulated in the [H-2] and [H-infinity] frameworks are derived. Moreover, the designed controllers are simulated to show that the desired performance metrics are met. / text

Στην παρούσα διδακτορική διατριβή αναλύθηκαν και μελετήθηκαν διάφορα συστήματα (ΗμΕ) προκειμένου να παρουσιαστεί η μοντελοποίηση τους. Κατά τη μοντελοποίηση αυτή, μελετήθη-καν τα χαρακτηριστικά τους και αναλύθηκε η συμπεριφορά τους. Στη συνέχεια, αναπτύχθηκαν νόμοι ελέγχου, οι οποίοι εφαρμόστηκαν στα συστήματα των ΗμΕ προκειμένου να επιτευχθεί ο έλεγχος της συμπεριφοράς τους. Αναλυτικότερα τα ζητήματα με τα οποία ασχολήθηκε η διατριβή αυτή παρουσιάζονται παρακάτω. Αρχικά πραγματοποιήθηκε η μοντελοποίηση των κάτωθι συστημάτων ΗμΕ: α) ένα σύστημα ΗμΕ του κυρίαρχου βαθμού ελευθερίας, β) ένα σύστημα ΗμΕ δύο βαθμών ελευθερίας και γ) ένα σύστημα ΗμΕ του κυρίαρ-χου βαθμού ελευθερίας στη μοντελοποίηση του οποίου λαμβάνεται υπόψιν η παρουσία του αέρα. Στη συνέχεια της διδακτορικής αυτής παρουσιάζονται και αναλύονται οι ελεγκτές οι οποίοι αναπτύχθηκαν και χρησιμοποιήθηκαν για τη μελέτη των συστημάτων αυτών και οι οποίοι είναι οι εξής: α) ένας Σθεναρός PID ελεγκτής, β) ένας Σθεναρός Η-infinity ελεγκτής, γ) ένας Σθεναρός Διακοπτικός PID ελεγκτής και δ) ένας H-infinity ελεγκτής προκαθορισμένων κερδών. Από την εφαρμογή των προτεινόμενων νόμων ελέγχου στα συστήματα ΗμΕ προκύπτουν τα αποτελέσματα της διδακτορικής αυτής διατριβής. Τα αποτελέσματα αυτά χωρίζονται σε δύο κατηγορίες. Αρχικά σε αυτά που αφορούν τη συμπεριφορά και τα χαρακτηριστικά των συστημάτων των ΗμΕ και στη συνέχεια σε αυτά τα οποία σχετίζονται με την εφαρμογή των νόμων ελέγχου στα συστήματα των ΗμΕ. Η κύρια συνεισφορά της διδακτορικής διατριβής αναφέρεται τόσο στην πρόταση νέων τεχνικών ελέγχου για τα συστήματα των ΗμΕ καθώς και η εφαρμογή με επιτυχία των τεχνικών αυτών στα συστήματα τα οποία μελετήθηκαν κατά τη διεκπόνηση της διατριβής. / In the present Phd thesis different systems of Electrostatic micro Actuators (EmA) have been presented and analyzed. During the modeling process the systems have been observed in order to provide the special characteristics and the special behavior of each model. In addition special control laws have been presented in order to control the movement of the movable parts of the EmAs. In general the main issues of this PhD thesis are presented in the sequel. Firstly the modeling of the following EmAs is presented: a) an EmA whose one plate is moving parallel to the x-axis b) an EmA whose plate is moving parallel to the x-axis and is also making an angular rotation c) an EmA system with squeezed film damping effects (presence of air between the moving surfaces). In the sequel the control laws that have been designed for the aforementioned systems are presented. The designed controllers are: a) a Robust PID controller b) a Robust Switching PID controller c) a robust Η-infinity controller and d) a robust Gain Scheduled H-infinity controller. In the last part of this thesis, the simulation results are presented concering both the behavior of the systems as well as the results provided by the application of the control laws.

The design of controllers subject to the nonlinear H-infinity criterion is explored. The plants to be controlled are the attitude motion of spacecraft, subject to some disturbance torque. Two cases are considered: the regulation about an inertially-fixed direction, and an Earth-pointing spacecraft in a circular orbit, subject to the gravity-gradient torque. The spacecraft attitude is described using the modified Rodrigues parameters. A series of controllers are designed using the nonlinear H-infinity control criterion, and are subsequently generated using a Taylor series expansion to approximate solutions of the relevant Hamilton-Jacobi equations. The controllers are compared, using both input-output and initial condition simulations. A proof is used to demonstrate that the linearized controller solves the H-infinity control problem for the inertial pointing problem when describing the plant using the modified Rodrigues parameters.

The design of controllers subject to the nonlinear H-infinity criterion is explored. The plants to be controlled are the attitude motion of spacecraft, subject to some disturbance torque. Two cases are considered: the regulation about an inertially-fixed direction, and an Earth-pointing spacecraft in a circular orbit, subject to the gravity-gradient torque. The spacecraft attitude is described using the modified Rodrigues parameters. A series of controllers are designed using the nonlinear H-infinity control criterion, and are subsequently generated using a Taylor series expansion to approximate solutions of the relevant Hamilton-Jacobi equations. The controllers are compared, using both input-output and initial condition simulations. A proof is used to demonstrate that the linearized controller solves the H-infinity control problem for the inertial pointing problem when describing the plant using the modified Rodrigues parameters.

abstract: This thesis addresses the design and control of three phase inverters. Such inverters are used to produce three-phase sinusoidal voltages and currents from a DC source. They are critical for injecting power from renewable energy sources into the grid. This is especially true since many of these sources of energy are DC sources (e.g. solar photovoltaic) or need to be stored in DC batteries because they are intermittent (e.g. wind and solar). Two classes of inverters are examined in this thesis. A control-centric design procedure is presented for each class. The first class of inverters is simple in that they consist of three decoupled subsystems. Such inverters are characterized by no mutual inductance between the three phases. As such, no multivariable coupling is present and decentralized single-input single-output (SISO) control theory suffices to generate acceptable control designs. For this class of inverters several families of controllers are addressed in order to examine command following as well as input disturbance and noise attenuation specifications. The goal here is to illuminate fundamental tradeoffs. Such tradeoffs include an improvement in the in-band command following and output disturbance attenuation versus a deterioration in out-of-band noise attenuation. A fundamental deficiency associated with such inverters is their large size. This can be remedied by designing a smaller core. This naturally leads to the second class of inverters considered in this work. These inverters are characterized by significant mutual inductances and multivariable coupling. As such, SISO control theory is generally not adequate and multiple-input multiple-output (MIMO) theory becomes essential for controlling these inverters. / Dissertation/Thesis / Masters Thesis Electrical Engineering 2015

abstract: The problem of systematically designing a control system continues to remain a subject of intense research. In this thesis, a very powerful control system design environment for Linear Time-Invariant (LTI) Multiple-Input Multiple-Output (MIMO) plants is presented. The environment has been designed to address a broad set of closed loop metrics and constraints; e.g. weighted H-infinity closed loop performance subject to closed loop frequency and/or time domain constraints (e.g. peak frequency response, peak overshoot, peak controls, etc.). The general problem considered - a generalized weighted mixed-sensitivity problem subject to constraints - permits designers to directly address and tradeoff multivariable properties at distinct loop breaking points; e.g. at plant outputs and at plant inputs. As such, the environment is particularly powerful for (poorly conditioned) multivariable plants. The Youla parameterization is used to parameterize the set of all stabilizing LTI proper controllers. This is used to convexify the general problem being addressed. Several bases are used to turn the resulting infinite-dimensional problem into a finite-dimensional problem for which there exist many efficient convex optimization algorithms. A simple cutting plane algorithm is used within the environment. Academic and physical examples are presented to illustrate the utility of the environment. / Dissertation/Thesis / M.S. Electrical Engineering 2013

Orientador: Alberto Luiz Serpa / Dissertação (mestrado) - Universidade Estadual de Campinas, Faculdade de Engenharia Mecânica / Made available in DSpace on 2018-08-27T04:19:56Z (GMT). No. of bitstreams: 1 HuamanOrtiz_RonaldRichard_M.pdf: 3700691 bytes, checksum: e0c35e9a16c6fd36ae433ab9a61c6cbb (MD5) Previous issue date: 2015 / Resumo: O projeto de sistemas de controle ativo de vibrações para estruturas flexíveis envolve a síntese de controladores que, geralmente, reduzem certos picos da resposta em frequência do sistema em malha fechada. Em alguns casos é requerido controlar unicamente um modo de vibrar específico do sistema em análise que pode estar associado a uma faixa de baixa, média ou alta frequência, o que demanda de um controle modal de vibrações. Neste trabalho, propõem-se três métodos alternativos para sintetizar controladores modais utilizando a teoria de controle H-infinito em uma configuração de controle por realimentação de saída. O primeiro método é implementado utilizando funções de ponderação as quais são introduzidas no problema de controle H-infinito para definir as características do controlador de maneira que este atenue a vibração do sistema na região em frequência correspondente ao modo que se deseja controlar (modo de interesse). O segundo método procura sintetizar controladores modais de menor ordem, utilizando uma planta reduzida. Essa planta reduzida contém unicamente a informação dinâmica do modo que se deseja controlar e é obtida através de uma transformação modal. O terceiro método procura melhorar o desempenho do controlador modal (conseguir uma maior redução da vibração do modo de interesse). Este método propõe sintetizar o controlador modal formulando um problema de otimização não linear onde as variáveis do controlador modal são as variáveis de otimização e a função objetivo é definida com valores específicos da resposta em frequência do sistema dinâmico. A solução deste problema de otimização é obtida utilizando o algoritmo de programação quadrática sequencial (SQP). Os três métodos são verificados utilizando o modelo de uma viga flexível engastada que é modelada através do método dos elementos finitos. Finalmente, os resultados obtidos são discutidos analisando as vantagens e desvantagens dos métodos propostos / Abstract: The design of active vibration control systems for flexible structures involves the tuning of controllers that reduce, generally, certain frequency resonance peaks of the close loop system. In some cases it is required to control a specific vibration mode of the system from a low, middle or high frequency range, demanding a modal vibration control. In this study it is proposed three alternative modal control methods using the H-infinity control theory in an output feedback control configuration. The first method is implemented using weighting functions which are introduced into the H-infinity control problem to define the characteristics of the controller so that it mitigates the system vibration in the frequency region that corresponds to a specific vibration mode (mode of interest). The second method attempts to synthesize lower order modal controllers, using a reduced plant. This reduced plant contains only the dynamic information of the vibration mode you want to control and is obtained through a modal transformation. The third method aims to improve the performance of the modal controller (to achieve a further reduction of the vibration mode of interest). This method proposes to synthesize the modal controller formulating a non-linear optimization problem where the variables of the modal controller are defined as the optimization variables and the objective function is defined with specific values of the frequency response of the dynamic system. The solution to this optimization problem is obtained using the sequential quadratic programming (SQP) algorithm. The three methods are verified using the model of a cantilever flexible beam that is modeled by the finite element method. Finally, the results are discussed considering the advantages and disadvantages of the proposed methods / Mestrado / Mecanica dos Sólidos e Projeto Mecanico / Mestre em Engenharia Mecânica