Experimental Active Vibration Control in Truss Structures Considering Uncertainties in System Parameters

Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)

Robust control to parametric uncertainties in smart structures using linear matrix inequalities

The study of algorithms for active vibrations control in flexible structures became an area of enormous interest, mainly due to the countless demands of an optimal performance of mechanical systems as aircraft and aerospace structures. Smart structures, formed by a structure base, coupled with piezoelectric actuators and sensor are capable to guarantee the conditions demanded through the application of several types of controllers. This article shows some steps that should be followed in the design of a smart structure. It is discussed: the optimal placement of actuators, the model reduction and the controller design through techniques involving linear matrix inequalities (LMI). It is considered as constraints in LMI: the decay rate, voltage input limitation in the actuators and bounded output peak (output energy). Two controllers robust to parametric variation are designed: the first one considers the actuator in non-optimal location and the second one the actuator is put in an optimal placement. The performance are compared and discussed. The simulations to illustrate the methodology are made with a cantilever beam with bonded piezoelectric actuators.

Optimal placement of sensors/actuators in truss structures with known disturbances

An important stage in the solution of active vibration control in flexible structures is the optimal placement of sensors and actuators. In many works, the positioning of these devices in systems governed for parameter distributed is, mainly, based, in controllability approach or criteria of performance. The positions that enhance such parameters are considered optimal. These techniques do not take in account the space variation of disturbances. An way to enhance the robustness of the control design would be to locate the actuators considering the space distribution of the worst case of disturbances. This paper is addressed to include in the formulation of problem of optimal location of sensors and piezoelectric actuators the effect of external disturbances. The paper concludes with a numerical simulation in a truss structure considering that the disturbance is applied in a known point a priori. As objective function the C norm system is used. The LQR (Linear Quadratic Regulator) controller was used to quantify performance of different sensors/actuators configurations.

Active control in flexible plates with piezoelectric actuators using linear matrix inequalities

The study of algorithms for active vibrations control in flexible structures became an area of enormous interest, mainly due to the countless demands of an optimal performance of mechanical systems as aircraft, aerospace and automotive structures. Smart structures, formed by a structure base, coupled with piezoelectric actuators and sensor are capable to guarantee the conditions demanded through the application of several types of controllers. The actuator/sensor materials are composed by piezoelectric ceramic (PZT - Lead Zirconate Titanate), commonly used as distributed actuators, and piezoelectric plastic films (PVDF-PolyVinyliDeno Floride), highly indicated for distributed sensors. The design process of such system encompasses three main phases: structural design; optimal placement of sensor/actuator (PVDF and PZT); and controller design. Consequently, for optimal design purposes, the structure, the sensor/actuator placement and the controller have to be considered simultaneously. This article addresses the optimal placement of actuators and sensors for design of controller for vibration attenuation in a flexible plate. Techniques involving linear matrix inequalities (LMI) to solve the Riccati's equation are used. The controller's gain is calculated using the linear quadratic regulator (LQR). The major advantage of LMI design is to enable specifications such as stability degree requirements, decay rate, input force limitation in the actuators and output peak bounder. It is also possible to assume that the model parameters involve uncertainties. LMI is a very useful tool for problems with constraints, where the parameters vary in a range of values. Once formulated in terms of LMI a problem can be solved efficiently by convex optimization algorithms.

Optimally distributed actuator placement and control for a slewing single-link flexible manipulator

A method is proposed for determining the optimal placement and controller design for multiple distributed actuators to reduce the vibrations of flexible structures. In particular, application of piezoceramic patches to a horizontally-slewing single-link flexible manipulator modeled using the assumed modes method is investigated. The optimization method uses simulated annealing and allows placement of any number of distributed actuators of unequal length, although piezoceramics of fixed equal lengths are used in the example. It also designs an linear-quadratic-regulator controller as part of the optimization procedure. The measures of performance used in the investigation to determine optimality are the total mass of the system and the time integral of the absolute value of the hub and tip position error. This study also varies the relative weightings for each of these performance measures to observe the effects on the controller designs and piezoceramic patch positions in the optimized solutions.

A framework for experimental determination of localised vertical pedestrian forces on full-scale structures using wireless attitude and heading reference systems

A major weakness among loading models for pedestrians walking on flexible structures proposed in recent years is the various uncorroborated assumptions made in their development. This applies to spatio-temporal characteristics of pedestrian loading and the nature of multi-object interactions. To alleviate this problem, a framework for the determination of localised pedestrian forces on full-scale structures is presented using a wireless attitude and heading reference systems (AHRS). An AHRS comprises a triad of tri-axial accelerometers, gyroscopes and magnetometers managed by a dedicated data processing unit, allowing motion in three-dimensional space to be reconstructed. A pedestrian loading model based on a single point inertial measurement from an AHRS is derived and shown to perform well against benchmark data collected on an instrumented treadmill. Unlike other models, the current model does not take any predefined form nor does it require any extrapolations as to the timing and amplitude of pedestrian loading. In order to assess correctly the influence of the moving pedestrian on behaviour of a structure, an algorithm for tracking the point of application of pedestrian force is developed based on data from a single AHRS attached to a foot. A set of controlled walking tests with a single pedestrian is conducted on a real footbridge for validation purposes. A remarkably good match between the measured and simulated bridge response is found, indeed confirming applicability of the proposed framework.

Topology optimization-based design of a compliant aircraft compliant aircraft wing for morphing leading and trailing edges

In this paper, we present a methodology for designing a compliant aircraft wing, which can morph from a given airfoil shape to another given shape under the actuation of internal forces and can offer sufficient stiffness in both configurations under the respective aerodynamic loads. The least square error in displacements, Fourier descriptors, geometric moments, and moment invariants are studied to compare candidate shapes and to pose the optimization problem. Their relative merits and demerits are discussed in this paper. The `frame finite element ground structure' approach is used for topology optimization and the resulting solutions are converted to continuum solutions. The introduction of a notch-like feature is the key to the success of the design. It not only gives a good match for the target morphed shape for the leading and trailing edges but also minimizes the extension of the flexible skin that is to be put on the airfoil frame. Even though linear small-displacement elastic analysis is used in optimization, the obtained designs are analysed for large displacement behavior. The methodology developed here is not restricted to aircraft wings; it can be used to solve any shape-morphing requirement in flexible structures and compliant mechanisms.

High Aspect Ratio (L/D) Riser Viv Prediction Using Wake Oscillator Model

A two-dimensional (2-D) vortex-induced vibration (VIV) prediction model for high aspect ratio (LID) riser subjected to uniform and sheared flow is studied in this paper. The nonlinear structure equations are considered. The near wake dynamics describing the fluctuating nature of vortex shedding is modeled using classical van der Pol equation. A new approach was applied to calibrate the empirical parameters in the wake oscillator model. Compared the predicted results with the experimental data and computational fluid dynamic (CFD) results. Good agreements are observed. It can be concluded that the present model can be used as simple computational tool in predicting some aspects of VIV of long flexible structures. (C) 2008 Elsevier Ltd. All rights reserved.

Dynamic fluid–structure interaction using finite volume unstructured mesh procedures

A three-dimensional finite volume, unstructured mesh (FV-UM) method for dynamic fluid–structure interaction (DFSI) is described. Fluid structure interaction, as applied to flexible structures, has wide application in diverse areas such as flutter in aircraft, wind response of buildings, flows in elastic pipes and blood vessels. It involves the coupling of fluid flow and structural mechanics, two fields that are conventionally modelled using two dissimilar methods, thus a single comprehensive computational model of both phenomena is a considerable challenge. Until recently work in this area focused on one phenomenon and represented the behaviour of the other more simply. More recently, strategies for solving the full coupling between the fluid and solid mechanics behaviour have been developed. A key contribution has been made by Farhat et al. [Int. J. Numer. Meth. Fluids 21 (1995) 807] employing FV-UM methods for solving the Euler flow equations and a conventional finite element method for the elastic solid mechanics and the spring based mesh procedure of Batina [AIAA paper 0115, 1989] for mesh movement. In this paper, we describe an approach which broadly exploits the three field strategy described by Farhat for fluid flow, structural dynamics and mesh movement but, in the context of DFSI, contains a number of novel features: • a single mesh covering the entire domain, • a Navier–Stokes flow, • a single FV-UM discretisation approach for both the flow and solid mechanics procedures, • an implicit predictor–corrector version of the Newmark algorithm, • a single code embedding the whole strategy.

Details of an integrated approach to three-dimensional dynamic fluid structure interaction

Fluid structure interaction, as applied to flexible structures, has wide application in diverse areas such as flutter in aircraft, wind response of buildings, flows in elastic pipes and blood vessels. Numerical modelling of dynamic fluid-structure interaction (DFSI) involves the coupling of fluid flow and structural mechanics, two fields that are conventionally modelled using two dissimilar methods, thus a single comprehensive computational model of both phenomena is a considerable challenge and until recently work in this area focused on one phenomenon and represented the behaviour of the other more simply. A single, finite volume unstructured mesh (FV-UM) spatial discretisation method has been employed on a single mesh for the entire domain. The Navier Stokes equations for fluid flow are solved using a SIMPLE type procedure and the Newmark b algorithm is employed for solving the dynamic equilibrium equations for linear elastic solid mechanics and mesh movement is achieved using a spring based mesh procedure for dynamic mesh movement. In the paper we describe a number of additional computation issues for the efficient and accurate modelling of three-dimensional, dynamic fluid-structure interaction problems.

Dynamic fluid-structure interactions using finite volume unstructured mesh procedures

A three-dimensional finite volume, unstructured mesh (FV-UM) method for dynamic fluid–structure interaction (DFSI) is described. Fluid structure interaction, as applied to flexible structures, has wide application in diverse areas such as flutter in aircraft, wind response of buildings, flows in elastic pipes and blood vessels. It involves the coupling of fluid flow and structural mechanics, two fields that are conventionally modelled using two dissimilar methods, thus a single comprehensive computational model of both phenomena is a considerable challenge. Until recently work in this area focused on one phenomenon and represented the behaviour of the other more simply. More recently, strategies for solving the full coupling between the fluid and solid mechanics behaviour have been developed. A key contribution has been made by Farhat et al. [Int. J. Numer. Meth. Fluids 21 (1995) 807] employing FV-UM methods for solving the Euler flow equations and a conventional finite element method for the elastic solid mechanics and the spring based mesh procedure of Batina [AIAA paper 0115, 1989] for mesh movement. In this paper, we describe an approach which broadly exploits the three field strategy described by Farhat for fluid flow, structural dynamics and mesh movement but, in the context of DFSI, contains a number of novel features: a single mesh covering the entire domain, a Navier–Stokes flow, a single FV-UM discretisation approach for both the flow and solid mechanics procedures, an implicit predictor–corrector version of the Newmark algorithm, a single code embedding the whole strategy.

A generic time and space accurate numerical approach to closely coupled fluid-structure interaction problems

Fluid structure interaction, as applied to flexible structures, has wide application in diverse areas such as flutter in aircraft, flow in elastic pipes and blood vessels and extrusion of metals through dies. However a comprehensive computational model of these multi-physics phenomena is a considerable challenge. Until recently work in this area focused on one phenomenon and represented the behaviour of the other more simply even to the extent in metal forming, for example, that the deformation of the die is totally ignored. More recently, strategies for solving the full coupling between the fluid and soild mechanics behaviour have developed. Conventionally, the computational modelling of fluid structure interaction is problematical since computational fluid dynamics (CFD) is solved using finite volume (FV) methods and computational structural mechanics (CSM) is based entirely on finite element (FE) methods. In the past the concurrent, but rather disparate, development paths for the finite element and finite volume methods have resulted in numerical software tools for CFD and CSM that are different in almost every respect. Hence, progress is frustrated in modelling the emerging multi-physics problem of fluid structure interaction in a consistent manner. Unless the fluid-structure coupling is either one way, very weak or both, transferring and filtering data from one mesh and solution procedure to another may lead to significant problems in computational convergence. Using a novel three phase technique the full interaction between the fluid and the dynamic structural response are represented. The procedure is demonstrated on some challenging applications in complex three dimensional geometries involving aircraft flutter, metal forming and blood flow in arteries.

La place de l’autonomie de l’apprenant en formation ouverte et à distance dans le contexte de l’enseignement supérieur ouest-africain

Les difficultés croissantes de l’enseignement supérieur en matière d’accessibilité aux formations et de disponibilité de filières de qualité, dans les pays en voie de développement de l’Afrique de l’Ouest notamment, conjuguées avec le développement vertigineux des technologies de l’information et de la communication (TIC), suscitent un grand espoir de faire de la formation à distance une solution alternative crédible des formations présentielles (OCDE, 2006). Or, si la littérature s’accorde à reconnaitre aux TIC et l’interactivité qu’elles procurent des facteurs favorisant l’apprentissage (Karsenti, 2006), la réalité du terrain éducatif lui impose de reconnaitre que non seulement la révolution de la formation ouverte et à distance (FOAD) n’est pas encore d’actualité (OCDE, 2006), mais qu’elle ne le sera que si, pour faire face à la distance transactionnelle, plus accrue en formation à distance, l’apprenant ne se contente plus d’apprendre, mais d’apprendre à apprendre, ce qui exige de lui des compétences d’autonomie. Or, malgré des décennies d’intérêt et d’investissement de la recherche, le développement de l’autonomie sur le terrain reste toujours marginal, les débats philosophiques ayant pris le pas sur la quête de solutions pratiques (Albero ,2003). La question de savoir comment les éducateurs de la FOAD utilisent les solutions existantes, censées favoriser l’autonomie de l’apprenant, telles certaines formes de tutorat et de travail de groupes, n’est pas sans intérêt, puisqu’elle permet de mieux comprendre le terrain cible et sa part de responsabilité dans cet insuccès de l’autonomie. S’inscrivant en droite ligne des travaux d’Albero (2003), la présente étude organise les principes d’autonomie suivant un cadre conceptuel privilégiant l’action et le développement, selon une dimension dynamique symbolisant l’importance du soutien à accorder à l’apprenant, une dimension topologique indiquant la nécessité pour ce soutien de prendre en compte les différents aspects sur lesquels l’apprenant peut exercer son autonomie et une dimension chronologique exprimant l’importance du désétayage. De façon pratique, cette étude, démarrée en 2009 dans le contexte de la FOAD du 2IE (Institut International des Ingénieurs de l’Eau et de l’Environnement), sis à Ouagadougou au Burkina Faso, s’organise en trois articles : le premier tente de comprendre si les conditions d’efficacité de la FOAD, selon les apprenants, formulent un besoin d’apprentissage en autonomie; le second tente de comprendre, à partir des propos des tuteurs, si l’encadrement des apprenants respecte les principes d’autonomie; enfin, le troisième article s’est penché, sur la base des intentions exprimées par les concepteurs, sur le respect des principes d’autonomie par les cours. L’éloignement des apprenants et l’objectif de comprendre leurs perceptions de la FOAD, nous ont fait préférer une approche de recherche de type mixte, à la fois qualitative pour mieux comprendre leur perception (Karsenti & Savoie-Zajc, 2004) et quantitative, pour tenir compte de leur éloignement. Pour la perception des éducateurs, nous avons opté pour une approche qualitative/descriptive plus appropriée dès que l’étude vise la compréhension du phénomène social abordé (Karsenti & Savoie-Zajc, 2004). Des résultats obtenus, la perception des 62 apprenants sur les 170 initialement invités par courriel à répondre au questionnaire, semble confirmer l’autonomie de l’apprenant comme une condition de leur réussite en FOAD. La demande des apprenants pour un soutien accru, malgré l’effort actuellement consenti par l’encadrement, effort reconnu par les apprenants eux-mêmes et qu’attestent les 10 tuteurs interviewés sur une quarantaine au 2IE, devrait, toutefois, inviter à la réflexion, puisque ne s’opposant pas réellement à un apprentissage en hétéronomie. À l’analyse, il apparait que l’insatisfaction des apprenants s’expliquerait par la non-prise en compte des différents aspects susceptibles d’influencer leur apprentissage. De plus, en nous référant aux entretiens avec les 11 concepteurs de cours sur un total de 30, il apparait que, bien que conscients de la nécessité d’adapter les cours au contexte de la FOAD, ni la modularité des contenus, ni la flexibilité de la structure des cours ne semblent être prises en compte. Au final, l’étude révèle l’urgence de lutter contre les habitudes acquises en formation présentielle et la nécessité d’employer des pédagogues professionnels formés pour une pédagogie d’autonomisation. Encore faudrait-il que l’autonomie soit véritablement consacrée par la littérature comme une praxis pour signifier qu’elle n’a d’autre fin qu’elle-même, et non comme une poiesis, pour dire que l’autonomie vise une production et cesserait dès que son objectif est atteint.

Desafios da adaptação institucional: um estudo do impacto da Lei de Consórcios Públicos no estado de São Paulo

A Lei nº 11.107/2005, que alterou o artigo 241 da Constituição Federal de 1988, intentou possibilitar aos consórcios a ampliação de seu potencial de atuação, pondo fim à sua fragilidade institucional. Permitindo sua constituição como pessoas jurídicas na figura de um consórcio de direito público ou de direito privado, buscou garantir, entre outras questões, o cumprimento das obrigações assumidas entre os membros e a participação dos três níveis da Federação. Sendo resultado de um processo de articulação em prol de sua regulamentação, a Lei de Consórcios Públicos representou a tentativa de aprimoramento do modelo de federalismo “cooperativo” no Brasil. No entanto, essas possibilidades ou ainda não foram utilizadas como fonte de recursos para algumas experiências ou têm ocorrido a uma velocidade mais lenta do que se esperava. Devido a esta alteração, supôs-se que a lei representaria um motor para o desenvolvimento de novos consórcios, bem como para o aperfeiçoamento das entidades já estabelecidas, que adotariam a nova personalidade de consórcio público. A partir desta problemática, o presente trabalho teve como objetivo realizar um estudo a respeito do processo de adaptação dos consórcios públicos à Lei nº 11.107/2005 à luz do neoinstitucionalismo histórico, com ênfase na investigação de três experiências de consórcios no estado de São Paulo, e que não se converteram para consórcios públicos nos moldes da lei. Em suma, foi possível concluir que, ainda que a lei apresente uma lista de possíveis vantagens, não criou instrumentos de aperfeiçoamento das experiências existentes, mas sim um novo arranjo de pactuação federativa. Essas experiências, que se desenvolveram ao longo de 40 anos sem instrumentos legais específicos para seu funcionamento – tendo, portanto, estruturas mais flexíveis –, apresentaram um comportamento de negação deliberada à adaptação aos instrumentos formais que a lei lhes apresentou. Dessa maneira, compreender de que modo os consórcios pré-existentes à Lei nº 11.107/2005 têm reconhecido as possibilidades dispostas por esse novo marco legal, de que maneira a trajetória desses arranjos pode influenciar em seu comportamento em relação à lei, e a própria trajetória da Lei de Consórcios Públicos, apresentou-se como um estudo ainda inexplorado e constitui-se como o norte principal da discussão neste trabalho.

Active flutter suppression in a 2-D airfoil using linear matrix inequalities techniques

Flutter is an in-flight vibration of flexible structures caused by energy in the airstream absorbed by the lifting surface. This aeroelastic phenomenon is a problem of considerable interest in the aeronautic industry, because flutter is a potentially destructive instability resulting from an interaction between aerodynamic, inertial, and elastic forces. To overcome this effect, it is possible to use passive or active methodologies, but passive control adds mass to the structure and it is, therefore, undesirable. Thus, in this paper, the goal is to use linear matrix inequalities (LMIs) techniques to design an active state-feedback control to suppress flutter. Due to unmeasurable aerodynamic-lag states, one needs to use a dynamic observer. So, LMIs also were applied to design a state-estimator. The simulated model, consists of a classical flat plate in a two-dimensional flow. Two regulators were designed, the first one is a non-robust design for parametric variation and the second one is a robust control design, both designed by using LMIs. The parametric uncertainties are modeled through polytopic uncertainties. The paper concludes with numerical simulations for each controller. The open-loop and closed-loop responses are also compared and the results show the flutter suppression. The perfomance for both controllers are compared and discussed. Copyright © 2006 by ABCM.