Este trabalho apresenta o controle de posição e orientação de um modelo não linear de Plataforma de Stewart com seis graus de liberdade construído no ambiente de sistemas multicorpos ADAMS® desenvolvido pela Mechanical Dynamics, Inc. O modelo não linear é exportado para o ambiente SIMULINK® desenvolvido pela MathWorks, Inc., onde o controle de posição e orientação é realizado a partir da linearização do modelo e a aplicação de um sistema seguidor com realimentação de estados. Utililiza-se, também o SIMULINK® para implementar a dinâmica de um sistema servoválvula e cilindro hidráulico com um servocontrole de pressão e assim simular o comportamento dinâmico de um simulador de vôo com acionamento hidráulico. A utilização destes pacotes comerciais visa obter uma economia de tempo e esforço na modelagem de sistemas mecânicos complexos e na programação para obtenção da resposta do sistema no tempo, além de facilitar a análise de várias configurações de Plataformas de Stewart / This work shows the position and orientation control of a non-linear model of a Stewart platform with six degree of freedom developed in the multibody systems environment ADAMS® (Mechanical Dynamics, Inc.). The non-linear model is exported to SIMULINK® (MathWorks, Inc.), where the position and orientation control is accomplished using the linear model and applied as a tracking-system with state-feedback. The SIMULINK® is also used to implement the dinamics of the servovalve and hydraulic cylinder with pressure-control servo and so simulate the dynamic behavior of the flight simulator with hydraulic drive. These commercial packages are used seeking to save time and effort in the modeling of complex mechanical systems and in the programming to get the time response of the system, facilitating the analysis of several Stewart Platforms configurations.

Nos últimos anos, tem havido grande interesse em estudar manipuladores paralelos, aplicados principalmente em simuladores de voo, com seis graus de liberdade. O interesse em estruturas cinemáticas paralelas é motivado por sua alta rigidez e excelente capacidade de posicionamento em relação às estruturas cinemáticas seriais. Além disso, como os atuadores são posicionados em uma base, eles podem ser aplicados em cargas pesadas e ainda apresentam baixo consumo de energia, tendo em vista que vários atuadores atuam simultaneamente no mesmo corpo. A presente tese apresenta o projeto de três controladores, sendo eles, o controlador H infinito com realimentação de saída, o controlador PID e o controlador Fuzzy, com isto, esta metodologia poderá ser empregada na construção de um futuro simulador de voo. O modelo dos atuadores foi obtido através de uma entrada degrau de tensão nos motores, medindo os seus deslocamentos através dos encoders acoplados, individualmente, a cada um dos respectivos eixos dos motores. Sabendo-se a relação de transmissão do mecanismo de movimento entre o motor e cada haste dos atuadores obtém-se o deslocamento de cada haste a partir da rotação de cada motor medida pelo correspondente encoder e com isso obtém-se o modelo matemático de cada atuador em conjunto com seu sistema de transmissão. Entretanto, na prática, cada atuador é ligeiramente diferente dos outros, o que leva a comportamento e desempenho diferentes entre si. Isso afeta o comportamento da plataforma fazendo com que a trajetória final desejada não possa ser seguida adequadamente, algo que é extremamente necessário em simuladores de voo. Assim, uma das contribuições importantes deste trabalho é, em primeiro lugar, apresentar uma metodologia de padronização das respostas dos atuadores de modo a que todos eles tenham no final, um comportamento igual o mais próximo possível, particularmente em termos de velocidade e de posicionamento. Com os dados da cinemática e da dinâmica da plataforma compondo o modelo completo do sistema foram realizadas várias simulações que aplicadas na plataforma de Stewart real validaram o modelo e mostraram a eficiência das técnicas de controle aplicadas no controle de posição e orientação da plataforma. Para validar o projeto da Plataforma de Stewart como uma possível base de movimento de um simulador de voo, foi implementada a dinâmica longitudinal e lateral de um Boeing 747-100, e com o auxilio de um sensor inercial Xsens® MTi-G, foram realizadas as medições dos ângulos de Euler da Plataforma. Os resultados obtidos pelos três controladores foram satisfatórios e ilustram o desempenho e a robustez da metodologia proposta. / In recent years there has been great interest in studying parallel manipulators, mainly applied in flight simulators, with six degrees of freedom. The interest in parallel kinematic structures is motivated by its high stiffness and excellent positioning capability in relation to serial kinematic structures. Furthermore, since the actuators are positioned on a base, they can handle heavy loads and also have low power consumption, considering that several actuators act on the same platform. This thesis presents the design of three controllers, which are, H-infinity controller with output feedback, PID controller and Fuzzy controller, so that this methodology can be employed in building a future flight simulator. The actuators models were obtained by a step voltage input to the engines and measuring their displacements by the encoders that are coupled to each of the respective axes of the motors. Knowing the relation from the motion transmission mechanism between the motor and the spindle of each actuator, the displacement of each spindle is obtained from the rotation of each motor measured by the corresponding encoder and thus we obtain the mathematical model of each actuator together with its transmission system. However, in practice, each actuator is slightly different from others, which leads to different behavior and performance of each. This affects the behavior of the platform making the final desired trajectory cannot be properly followed something that is extremely necessary in flight simulators. Thus, one of the important contributions of this work is first to present a methodology to standardize the actuators responses so that they all have in the end a behavior equal a close as possible, particularly in terms of velocity and positioning. With the kinematics data and platform dynamics composing the complete system model, several simulations applied to the real Stewart Platform validate the model and show the effectiveness of control techniques applied to control the position and orientation of the platform. In order to validate the Stewart Platform design as a possible base for a motion flight simulator, the longitudinal and lateral dynamics of a Boeing 747-100 model were implemented, and with the aid of an inertial sensor Xsens® MTi-G, measurements of the Euler angles of the platform were performed. The results obtained by the three controllers were satisfactory and illustrate the performance and robustness of the proposed methodology.

Orientador: Donato Giorgio Torrieri / Dissertação (mestrado) - Universidade Estadual de Campinas, Instituto de Física Gleb Wataghin / Made available in DSpace on 2018-08-31T06:57:06Z (GMT). No. of bitstreams: 1 Coelho_DavidMontenegro_M.pdf: 2238497 bytes, checksum: 78f745f9d544a31d97a2d7a80b7dc505 (MD5) Previous issue date: 2016 / Resumo: O interesse científico cresceu após confirmado por testes experimentais o comportamento do Plasma de Quark-Glúon como um fluido quase perfeito no LHC e RHIC. O objetivo desse trabalho é fornecer as bases teóricas da Effective Field Theory (EFT) na abordagem da Hidrodinâmica, pois vários recursos não-triviais na dinâmica relativística dos fluidos são claramente explicados por esse formalismo. Problemas teóricos na EFT sugerem a inclusão de uma nova formulação do Princípio de Hamilton compatível com o princípio da causalidade, através do Closed-Time-Path. Após resolvido esse problema, alcançamos o requisito necessário para derivar a hidrodinâmica dissipativa em altas ordens por meio da ação. Assim, conseguimos caracterizar a Lagrangeana de Navier-Stokes ao introduzir a quebra de simetria na preservação do difeomorfismo pelo volume por meio do termo $B^{-1}_{IJ}$. No entanto, uma análise pelo método de Ostrogradski levou à supressão dessa equação, através da inclusão da Lagrangeana de Israel-Stewart na expansão que é justificada por meios de argumentos de estabilidade e causalidade. Por fim, propomos uma variável $X_{IJ}$ na Lagrangeana de Israel-Stewart, simétrica, anisotrópica e dependente das condições iniciais que juntamente com os já estabelecidos graus de liberdade de campo, formam a base para a derivação bottom-up em altas ordens da EFT e propicia medidas para estudar turbulência e instabilidade no vácuo e outras situações que chegam da relação entre graus de liberdade macroscópico e microscópico / Abstract: Scientific interest grew after the behavior of the quark-gluon Plasma as a nearly perfect fluid in the LHC and RHIC. The objective of this dissertation is offer support to use the Effective Field Theory (EFT) approach to study hydrodynamics because many non-trivial features in relativistic fluid dynamics are clearly explained by this Lagrangian formalism. Theoretical problems in EFT considering by including a new formulation of the Hamiltonian principle that is compatible with the principle of causality for non-conservative field through the Closed-Time-Path formalism. After solving this problem, we reached requirement to derive the dissipative hydrodynamics in higher orders of action. We were able to characterize Navier-Stokes' Lagrangian by introducing the symmetry breaking of preserving diffeomorphism through the volume with the term $B^{-1}_{IJ} $ to the Lagrangian of Navier-Stokes. An analyse of Ostrogradski's method led to the removal of equation by including the Israel-Stewart term in the Lagrangian expansion that provides an extra justification by means of symmetry and causality arguments. Finally, we propose a variable $ X_ {IJ} $, Israel-Stewart's Lagrangian, symmetric, anisotropic and dependent on initial conditions together with an established degree of freedom of the field, which form the basis for the derivation of higher orders of the bottom up and promote steps to the study of turbulence by instability in the vacuum, and other situations arising from the relationship between macroscopic and microscopic degrees of freedom / Mestrado / Física / Mestre em Física / 147435/2014-5 / CNPQ

Around 40 million people around the world have amputated parts of their bodies. Prostheses are widely used to support their daily behavior. However, about 35% of amputees refuse to use the prostheses due to comfort problems. SocketSense is an EU research project that aims to improve the situation. The Stewart platform (SP) is used as the model of the prototype. The SP could reproduce the comparing forces and torques interior the socket-to-stump interface, given prerecorded movement information of an amputee’s walk cycle. However, previous work controls SP based on inputting some simple reference trajectories ,or for radar, satellite and vehicle use-cases. This  thesis is committed to designing and implementing a control algorithm for the SP to control the socket. The task is divided into two main parts: simulation on Matlab/Simulink and implementation on Linux/ROS, and each part is split into several steps. Firstly, the PID control algorithm is selected and developed for the SP. Secondly, the simulation model is designed and built on Matlab/Simulink. Based on the simulation model, the control algorithm is implemented into the model. Then, the results of simulation are obtained. After that, the SP model is built on Linux/ROS. Then, the model is connected and communicated with the real platform. Finally, the output data and system performance are analysed in terms of control performance, real-time performance, anti-noise performance, etc. The results show that both the simulation and the actual platform system can follow the reference trajectory well. Although there is noise in the results of the actual platform, the noise is suppressed to a great extent by Kalman filter. / Runt 40 miljoner människor runtom i världen har amputerat delar av sina kroppar. Proteser används ofta för att stödja deras dagliga beteende. Emellertid vägrar cirka 35% av amputerade att använda proteserna på grund av komfort problem. SocketSense är ett EU-forsknings projekt som syftar till att förbättra situationen. SP används som modell för prototypen. SP skulle kunna återskapa de jämförande krafterna och vridmomenten inuti gränssnittet uttag-till-stump, givet förinspelad rörelseinformation om en amputerads gångcykel. Tidigare arbete styr dock SP baserat på att ange några enkla referensbanor, eller för radar-, satellit-och fordonsanvändningsfall. Detta examensarbete syftar till att designa och implementera en kontroll algoritmför SP för att styra socket. Uppgiften är uppdelad i två huvuddelar: simulering på Matlab/ Simulink och implementering på Linux/ROS, och varje del är uppdelad i flera steg. Först väljs och utvecklas PID-kontrollalgoritmen för SP. För det andra är simuleringsmodellen designad och byggd på Matlab/ Simulink. Baserat på simuleringsmodellen implementeras styralgoritmen i modellen. Därefter erhålls resultaten av simuleringen. Därefter är SP-modellen byggd på Linux/ROS. Sedan kopplas modellen ihop och kommuniceras med den verkliga plattformen. Slutligen analyseras utdata och systemprestanda i termer av kontrollprestanda, realtidsprestanda, anti-brusprestanda, etc. Result visar att både simuleringen och det faktiska plattformssystemet kan följa referensbanan väl. Även om det finns brus i resultaten av själva plattformen, dämpas bruset i hög grad av Kalman-filter.

The work performed in this thesis involves the study of human hip joint kinematics and load analysis. Such analyses are very useful for investigating mobility and natural functionality as well as the variation in motion due to replacement implants. The objective of this study is to design, build and testing of a universal human joint simulator that is configurable to hold several human joints and easily programmable to create the required motion. This was performed by creating a Stewart Platform, which is capable of moving in all six degrees of freedom; the maximum number needed by any human joint. Many specific human joint simulators are available on the market for simulating all major human limbs. These are used for wear testing replacement joints by using high load repetitive motion. These systems have a predetermined limit degree of movement and are very expensive; if one wanted to emulate another joint, one would have to purchase a whole new system. This novel system compromises of a three-phase power supply, Control Area Network with six actuators and drivers, a force reading clamp with strain gauges and data logger. A user friendly computer program was developed that is able to derive joint movement data from two inputs and replicating the movement by driving the platform, as well as recording force and displacement data from the joint. The product would be marketed towards biomechanical researchers and implant designers. Verification of this system was performed by simulating the human hip joint. A known combination of kinematic and force data were inputted into the system for nine different types of activities. The resultant force and joint centre displacement was then compared to see how well the system perform in comparison to the inputted data from a previous study. The outcome of this project is a fully functional machine and configurable program that can create movement data at varying speeds and body weights; which is also able to drive the human joint simulator. The design also costs a fraction of any industrial joint simulator. It is hoped that the simulator will allow easier study of both the kinematics and load analysis within the human joints, with the intent on aiding investigation into mobility and functionality; as well as variation in motion caused by a replacement implant.

In this work, we investigate the active vibration isolation and damping of sensitive equipment. Several single-axis isolation techniques are analyzed and tested. A comparison between the sky-hook damper, integral force feedback, inertial velocity feedback and LagLead control techniques is conducted using several practical examples. The study of single-axis systems has been developed and used to build a six-axis isolator. A six degrees of freedom active isolator based on Stewart platform has been designed manufactured and tested for the purpose of active vibration isolation of sensitive payloads in space applications. This six-axis hexapod is designed according to the cubic configuration; it consists of two triangular parallel plates connected to each other by six active legs orthogonal to each other; each leg consists of a voice coil actuator, a force sensor and two flexible joints. Two different control techniques have been tested to control this isolator : integral force feedback and Lag-Lead compensator, the two techniques are based on force feedback and are applied in a decentralized manner. A micro-gravity parabolic flight test has been clone to test the isolator in micro-gravity environment. ln the context of this research, another hexapod has been produced ; a generic active damping and precision painting interface based on Stewart platform. This hexapod consists of two parallel plates connected to each other by six active legs configured according to the cubic architecture. Each leg consists of an amplified piezoelectric actuator, a force sensor and two flexible joints. This Stewart platform is addressed to space applications where it aims at controlling the vibrations of space structures while connecting them rigidly. The control technique used here is the decentralized integral force feedback.

The safety and functionality of engineering systems can be affected adversely by faults or wear in system components. Therefore, methods for detecting such faults/wear and ameliorating their effects to avoid system failure are important. Designing schemes for the detection and diagnosis of faults is becoming increasingly important in engineering due to the complexity of modern industrial systems and growing demands for quality, cost efficiency, reliability, and the safety issue. In safety/mission critical applications, fault detection can be combined with accommodation/reconfiguration (after a fault) to achieve fault tolerance allowing the system to complete or abort its function in a way that is sub-optimal but does achieve the design objective. This thesis discusses research carried-out on the development and validation of a model-based fault detection and isolation (FDI) system for a pneumatically actuated Stewart platform. The Stewart-Gough platform provides six degrees of freedom consisting of three translational and three rotational degrees of freedom (x, y, z, pitch, roll, & yaw). As these platforms can be fast acting (rapid motion) and can handle reasonable loads, they can become dangerous, especially when fault(s) in the platform mechanism, drivetrain or control system occur. Therefore, as a safety critical application it is imperative that fault tolerant schemes are applied in order to provide a safe working environment. The design concept of the FDI scheme for the full Stewart-Gough platform is first designed using a single cylinder set-up. This modular concept is adopted so that a robust fault tolerant control scheme can be designed basically off-line (i.e. not attached to the Stewart Gough platform). This approach is adopted as requirements are easier to understand using a single cylinder set-up. The modular design approach subdivides the whole system into smaller sections (modules) that can be independently created and then used in the complete Stewart-Gough platform. The main contributions of the work are that a pneumatically actuated Stewart-Gough platform has been designed, built, and commissioned. A mathematical model has been developed and has been validated against experimental results. Two control approaches have been designed and compared. A fundamental comparative study of parity equations and Kalman filter observer banks for fault detection in pneumatic actuators has been conducted. The parity equations and Kalman filter approaches have been extended to provide a combined fault detection scheme. The FDI and control schemes have been combined in a modular Fault Tolerant Control (FTC) scheme for a pneumatic cylinder. The resulting FTC scheme has been validated by experimentation and demonstrated on the single cylinder test rig. The FTC scheme has been extended to all 6 cylinders (and including fault management at top level) of Stewart-Gough platform. The FTC scheme has been validated by experimentation and demonstrated on the Stewart-Gough platform test rig.

Předkládaná práce se zabývá návrhem modelu dynamiky paralelního manipulátoru optimálního pro účely návrhu řízení. Zvolený přístup je založen na modelování dynamiky systému v simulačním prostředí Matlab SimMechanics následovaném linearizací modelu. Výsledný stavový lineární model mimo jiné umožňuje snadné posouzení řiditelnosti a pozorovatelnosti modelu. Díky své relativní jednoduchosti je model také výpočetně nenáročný. Přístup je demonstrován na návrhu dvouvrstvého řízení SimMechanics modelu Stewartovy platformy, na kterém bylo následně navržené řízení úspěšně testováno. Podstatná část práce obsahuje přístup k modelování neurčitých parametrů dynamického modelu Stewartovy platformy a stejnosměrného motoru Maxon RE 35 a jeho výsledky. Předložený přístup je založen na modelování parametrické neurčitosti způsobem, kdy je neurčitost definována individuálně pro jednotlivé prvky stavových matic modelu. Samotná neurčitost je potom určena rozdílem mezi jednotlivými parametry příslušných matic nominálního modelu a modelu se stanovenou maximální neurčitostí parametrů. Výsledný neurčitostní model je vzhledem ke své stavové reprezentaci vhodný pro návrh regulátoru založeném na metodách návrhu robustního řízení, například minimalizaci normy H-nekonečno. Popsaná metoda byla použita pro kompenzaci posunu mezi pracovními body, okolo kterých je prováděna linearizace a pro kompenzaci nepřesnosti modelování vybraných parametrů modelů Stewartovy platformy a stejnosměrného motoru. Získané modely (v prostředí SimMechanics a neurčitostní model) byly experimentálně porovnány s chováním jednoho z lineárních pohonů Stewartovy platformy. Rozdíl v datech obdržených ze simulace v prostředí SimMechanics a naměřených na reálném stroji byl téměř kompletně pokryt neurčitostním modelem. Prezentovaná metoda neurčitostního modelování je velice univerzální a aplikovatelná na libovolný stavový model.

In this paper, I consider the success of Jonathan Swift’s The Drapier’s Letters and Jon Stewart’s The Daily Show in changing the political climate of the world around them. By analyzing the political background of America in the 2000s and the Irish reaction to William Woods’ patent in the 1720s, I prove the influence of Stewart and Swift’s satire. I then analyze the specific tactics each employs in order to achieve an audience and influence change, concluding by comparing the similar tactics that each use, including persona, irony, and humor as a veil of serious intent.

Thesis advisor: William Stanwood / The Daily Show with Jon Stewart's ascendance into the mainstream consciousness has reached a point where many not only consider it to be a source of news, but also Stewart to be one of the most respected and important journalists in the country. This study investigated The Daily Show’s impact on the general public using the theoretical framework of agenda-setting. After grounding the study in existing scholarly research, data, content and textual analyses were performed on 12 Daily Show episodes, as well as data analysis on the corresponding network news broadcasts. It was then concluded that The Daily Show has no significant impact on what people think about no matter what variables were analyzed. Thus, Stewart likely has been right all along in his claim that he and his team are not journalists – rather, they are merely producing a comedy show that happens to involve news and parodies news broadcasts. / Thesis (BA) — Boston College, 2011. / Submitted to: Boston College. College of Arts and Sciences. / Discipline: College Honors Program. / Discipline: Communication Honors Program. / Discipline: Communication.