Estudo da comunicação de um compensador série para rede de distribuição com o centro de controle utilizando tecnologia GPRS

Pós-graduação em Engenharia Elétrica - FEIS

Um novo sistema de refrigeração com controle de temperatura, compressor aberto, máquina de indução trifásica com velocidade variável e correção ativa do fator de potência do estágio de entrada

Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)

Description of the attainable sets of one-dimensional differential inclusions

The role played by the attainable set of a differential inclusion, in the study of dynamic control systems and fuzzy differential equations, is widely acknowledged. A procedure for estimating the attainable set is rather complicated compared to the numerical methods for differential equations. This article addresses an alternative approach, based on an optimal control tool, to obtain a description of the attainable sets of differential inclusions. In particular, we obtain an exact delineation of the attainable set for a large class of nonlinear differential inclusions.

Application of H-infinity Theory to a 6 DOF Flight Simulator Motion Base

The purpose of this study is to apply inverse dynamics control for a six degree of freedom flight simulator motion system. Imperfect compensation of the inverse dynamic control is intentionally introduced in order to simplify the implementation of this approach. The control strategy is applied in the outer loop of the inverse dynamic control to counteract the effects of imperfect compensation. The control strategy is designed using H-infinity theory. Forward and inverse kinematics and full dynamic model of a six degrees of freedom motion base driven by electromechanical actuators are briefly presented. Describing function, acceleration step response and some maneuvers computed from the washout filter were used to evaluate the performance of the controllers.

Application of H∞ theory to a 6 DOF flight simulator motion base

The purpose of this study is to apply inverse dynamics control for a six degree of freedom flight simulator motion system. Imperfect compensation of the inverse dynamic control is intentionally introduced in order to simplify the implementation of this approach. The control strategy is applied in the outer loop of the inverse dynamic control to counteract the effects of imperfect compensation. The control strategy is designed using H∞ theory. Forward and inverse kinematics and full dynamic model of a six degrees of freedom motion base driven by electromechanical actuators are briefly presented. Describing function, acceleration step response and some maneuvers computed from the washout filter were used to evaluate the performance of the controllers.

Procedimenti di ottimizzazione di sistemi smorzati

La presente tesi riguarda lo studio di procedimenti di ottimizzazione di sistemi smorzati. In particolare, i sistemi studiati sono strutture shear-type soggette ad azioni di tipo sismico impresse alla base. Per effettuare l’ottimizzazione dei sistemi in oggetto si agisce sulle rigidezze di piano e sui coefficienti di smorzamento effettuando una ridistribuzione delle quantità suddette nei piani della struttura. È interessante effettuare l’ottimizzazione di sistemi smorzati nell’ottica della progettazione antisismica, in modo da ridurre la deformata della struttura e, conseguentemente, anche le sollecitazioni che agiscono su di essa. Il lavoro consta di sei capitoli nei quali vengono affrontate tre procedure numerico-analitiche per effettuare l’ottimizzazione di sistemi shear-type. Nel primo capitolo si studia l’ottimizzazione di sistemi shear-type agendo su funzioni di trasferimento opportunamente vincolate. In particolare, le variabili di progetto sono le rigidezze di piano, mentre i coefficienti di smorzamento e le masse di piano risultano quantità note e costanti durante tutto il procedimento di calcolo iterativo; per effettuare il controllo dinamico della struttura si cerca di ottenere una deformata pressoché rettilinea. Tale condizione viene raggiunta ponendo le ampiezze delle funzioni di trasferimento degli spostamenti di interpiano pari all’ampiezza della funzione di trasferimento del primo piano. Al termine della procedura si ottiene una ridistribuzione della rigidezza complessiva nei vari piani della struttura. In particolare, si evince un aumento della rigidezza nei piani più bassi che risultano essere quelli più sollecitati da una azione impressa alla base e, conseguentemente, si assiste ad una progressiva riduzione della variabile di progetto nei piani più alti. L’applicazione numerica di tale procedura viene effettuata nel secondo capitolo mediante l’ausilio di un programma di calcolo in linguaggio Matlab. In particolare, si effettua lo studio di sistemi a tre e a cinque gradi di libertà. La seconda procedura numerico-analitica viene presentata nel terzo capitolo. Essa riguarda l’ottimizzazione di sistemi smorzati agendo simultaneamente sulla rigidezza e sullo smorzamento e consta di due fasi. La prima fase ricerca il progetto ottimale della struttura per uno specifico valore della rigidezza complessiva e dello smorzamento totale, mentre la seconda fase esamina una serie di progetti ottimali in funzione di diversi valori della rigidezza e dello smorzamento totale. Nella prima fase, per ottenere il controllo dinamico della struttura, viene minimizzata la somma degli scarti quadratici medi degli spostamenti di interpiano. Le variabili di progetto, aggiornate dopo ogni iterazione, sono le rigidezze di piano ed i coefficienti di smorzamento. Si pone, inoltre, un vincolo sulla quantità totale di rigidezza e di smorzamento, e i valori delle rigidezze e dei coefficienti di smorzamento di ogni piano non devono superare un limite superiore posto all’inizio della procedura. Anche in questo caso viene effettuata una ridistribuzione delle rigidezze e dei coefficienti di smorzamento nei vari piani della struttura fino ad ottenere la minimizzazione della funzione obiettivo. La prima fase riduce la deformata della struttura minimizzando la somma degli scarti quadrarici medi degli spostamenti di interpiano, ma comporta un aumento dello scarto quadratico medio dell’accelerazione assoluta dell’ultimo piano. Per mantenere quest’ultima quantità entro limiti accettabili, si passa alla seconda fase in cui si effettua una riduzione dell’accelerazione attraverso l’aumento della quantità totale di smorzamento. La procedura di ottimizzazione di sistemi smorzati agendo simultaneamente sulla rigidezza e sullo smorzamento viene applicata numericamente, mediante l’utilizzo di un programma di calcolo in linguaggio Matlab, nel capitolo quattro. La procedura viene applicata a sistemi a due e a cinque gradi di libertà. L’ultima parte della tesi ha come oggetto la generalizzazione della procedura che viene applicata per un sistema dotato di isolatori alla base. Tale parte della tesi è riportata nel quinto capitolo. Per isolamento sismico di un edificio (sistema di controllo passivo) si intende l’inserimento tra la struttura e le sue fondazioni di opportuni dispositivi molto flessibili orizzontalmente, anche se rigidi in direzione verticale. Tali dispositivi consentono di ridurre la trasmissione del moto del suolo alla struttura in elevazione disaccoppiando il moto della sovrastruttura da quello del terreno. L’inserimento degli isolatori consente di ottenere un aumento del periodo proprio di vibrare della struttura per allontanarlo dalla zona dello spettro di risposta con maggiori accelerazioni. La principale peculiarità dell’isolamento alla base è la possibilità di eliminare completamente, o quantomeno ridurre sensibilmente, i danni a tutte le parti strutturali e non strutturali degli edifici. Quest’ultimo aspetto è importantissimo per gli edifici che devono rimanere operativi dopo un violento terremoto, quali ospedali e i centri operativi per la gestione delle emergenze. Nelle strutture isolate si osserva una sostanziale riduzione degli spostamenti di interpiano e delle accelerazioni relative. La procedura di ottimizzazione viene modificata considerando l’introduzione di isolatori alla base di tipo LRB. Essi sono costituiti da strati in elastomero (aventi la funzione di dissipare, disaccoppiare il moto e mantenere spostamenti accettabili) alternati a lamine in acciaio (aventi la funzione di mantenere una buona resistenza allo schiacciamento) che ne rendono trascurabile la deformabilità in direzione verticale. Gli strati in elastomero manifestano una bassa rigidezza nei confronti degli spostamenti orizzontali. La procedura di ottimizzazione viene applicata ad un telaio shear-type ad N gradi di libertà con smorzatori viscosi aggiunti. Con l’introduzione dell’isolatore alla base si passa da un sistema ad N gradi di libertà ad un sistema a N+1 gradi di libertà, in quanto l’isolatore viene modellato alla stregua di un piano della struttura considerando una rigidezza e uno smorzamento equivalente dell’isolatore. Nel caso di sistema sheat-type isolato alla base, poiché l’isolatore agisce sia sugli spostamenti di interpiano, sia sulle accelerazioni trasmesse alla struttura, si considera una nuova funzione obiettivo che minimizza la somma incrementata degli scarti quadratici medi degli spostamenti di interpiano e delle accelerazioni. Le quantità di progetto sono i coefficienti di smorzamento e le rigidezze di piano della sovrastruttura. Al termine della procedura si otterrà una nuova ridistribuzione delle variabili di progetto nei piani della struttura. In tal caso, però, la sovrastruttura risulterà molto meno sollecitata in quanto tutte le deformazioni vengono assorbite dal sistema di isolamento. Infine, viene effettuato un controllo sull’entità dello spostamento alla base dell’isolatore perché potrebbe raggiungere valori troppo elevati. Infatti, la normativa indica come valore limite dello spostamento alla base 25cm; valori più elevati dello spostamento creano dei problemi soprattutto per la realizzazione di adeguati giunti sismici. La procedura di ottimizzazione di sistemi isolati alla base viene applicata numericamente mediante l’utilizzo di un programma di calcolo in linguaggio Matlab nel sesto capitolo. La procedura viene applicata a sistemi a tre e a cinque gradi di libertà. Inoltre si effettua il controllo degli spostamenti alla base sollecitando la struttura con il sisma di El Centro e il sisma di Northridge. I risultati hanno mostrato che la procedura di calcolo è efficace e inoltre gli spostamenti alla base sono contenuti entro il limite posto dalla normativa. Giova rilevare che il sistema di isolamento riduce sensibilmente le grandezze che interessano la sovrastruttura, la quale si comporta come un corpo rigido al di sopra dell’isolatore. In futuro si potrà studiare il comportamento di strutture isolate considerando diverse tipologie di isolatori alla base e non solo dispositivi elastomerici. Si potrà, inoltre, modellare l’isolatore alla base con un modello isteretico bilineare ed effettuare un confronto con i risultati già ottenuti per il modello lineare.

Effect of knee joint angle on motor unit synchronization

Activity of the vasti has been argued to vary through knee range of movement due to changes in passive support of the patellofemoral joint and the relative contribution of these muscles to knee extension. Efficient function of the knee is dependent on optimal control of the patellofemoral joint, largely through coordinated activity of the medial and lateral quadriceps. Motor unit synchronization may provide a mechanism to coordinate the activity of vastus medialis (VMO) and vastus lateralis (VL), and may be more critical in positions of reduced passive support for the patellofemoral joint (i.e., full extension). Therefore, the aim of this study was to determine whether the degree of motor unit synchronization between the vasti muscles is dependent on joint angle. Electromyographic (EMG) recordings of single motor unit action potentials (MUAPs) were made from VMO and multiunit recordings from VL during isometric contractions of the quadriceps at 0 degrees, 30 degrees, and 60 degrees of knee flexion. The degree of synchronization between motor unit firing was evaluated by identification of peaks in the rectified EMG averages of VL, triggered from MUA-Ps in VMO. The proportion of cases in which there was a significant peak in the triggered averages was calculated. There was no significant difference in the degree of synchronization between the vasti at different knee angles (p = 0.57). These data suggest that this basic coordinative mechanism between the vasti muscles is controlled consistently throughout knee range of motion, and is not augmented at specific angles where the requirement for dynamic control of stability is increased. (D 2006 Orthopaedic Research Society. Published by Wiley Periodicals, Inc.

Resonant cavity Fibre Bragg grating sensor interrogation

This thesis presents a novel high-performance approach to time-division-multiplexing (TDM) fibre Bragg grating (FBG) optical sensors, known as the resonant cavity architecture. A background theory of FBG optical sensing includes several techniques for multiplexing sensors. The limitations of current wavelength-division-multiplexing (WDM) schemes are contrasted against the technological and commercial advantage of TDM. The author’s hypothesis that ‘it should be possible to achieve TDM FBG sensor interrogation using an electrically switched semiconductor optical amplifier (SOA)’ is then explained. Research and development of a commercially viable optical sensor interrogator based on the resonant cavity architecture forms the remainder of this thesis. A fully programmable SOA drive system allows interrogation of sensor arrays 10km long with a spatial resolution of 8cm and a variable gain system provides dynamic compensation for fluctuating system losses. Ratiometric filter- and diffractive-element spectrometer-based wavelength measurement systems are developed and analysed for different commercial applications. The ratiometric design provides a low-cost solution that has picometre resolution and low noise using 4% reflective sensors, but is less tolerant to variation in system loss. The spectrometer design is more expensive, but delivers exceptional performance with picometre resolution, low noise and tolerance to 13dB system loss variation. Finally, this thesis details the interrogator’s peripheral components, its compliance for operation in harsh industrial environments and several examples of commercial applications where it has been deployed. Applications include laboratory instruments, temperature monitoring systems for oil production, dynamic control for wind-energy and battery powered, self-contained sub-sea strain monitoring.

Mechanochemistry for Active Materials and Devices

The coupling of mechanical stress fields in polymers to covalent chemistry (polymer mechanochemistry) has provided access to previously unattainable chemical reactions and polymer transformations. In the bulk, mechanochemical activation has been used as the basis for new classes of stress-responsive polymers that demonstrate stress/strain sensing, shear-induced intermolecular reactivity for molecular level remodeling and self-strengthening, and the release of acids and other small molecules that are potentially capable of triggering further chemical response. The potential utility of polymer mechanochemistry in functional materials is limited, however, by the fact that to date, all reported covalent activation in the bulk occurs in concert with plastic yield and deformation, so that the structure of the activated object is vastly different from its nascent form. Mechanochemically activated materials have thus been limited to “single use” demonstrations, rather than as multi-functional materials for structural and/or device applications. Here, we report that filled polydimethylsiloxane (PDMS) elastomers provide a robust elastic substrate into which mechanophores can be embedded and activated under conditions from which the sample regains its original shape and properties. Fabrication is straightforward and easily accessible, providing access for the first time to objects and devices that either release or reversibly activate chemical functionality over hundreds of loading cycles.

While the mechanically accelerated ring-opening reaction of spiropyran to merocyanine and associated color change provides a useful method by which to image the molecular scale stress/strain distribution within a polymer, the magnitude of the forces necessary for activation had yet to be quantified. Here, we report single molecule force spectroscopy studies of two spiropyran isomers. Ring opening on the timescale of tens of milliseconds is found to require forces of ~240 pN, well below that of previously characterized covalent mechanophores. The lower threshold force is a combination of a low force-free activation energy and the fact that the change in rate with force (activation length) of each isomer is greater than that inferred in other systems. Importantly, quantifying the magnitude of forces required to activate individual spiropyran-based force-probes enables the probe behave as a “scout” of molecular forces in materials; the observed behavior of which can be extrapolated to predict the reactivity of potential mechanophores within a given material and deformation.

We subsequently translated the design platform to existing dynamic soft technologies to fabricate the first mechanochemically responsive devices; first, by remotely inducing dielectric patterning of an elastic substrate to produce assorted fluorescent patterns in concert with topological changes; and second, by adopting a soft robotic platform to produce a color change from the strains inherent to pneumatically actuated robotic motion. Shown herein, covalent polymer mechanochemistry provides a viable mechanism to convert the same mechanical potential energy used for actuation into value-added, constructive covalent chemical responses. The color change associated with actuation suggests opportunities for not only new color changing or camouflaging strategies, but also the possibility for simultaneous activation of latent chemistry (e.g., release of small molecules, change in mechanical properties, activation of catalysts, etc.) in soft robots. In addition, mechanochromic stress mapping in a functional actuating device might provide a useful design and optimization tool, revealing spatial and temporal force evolution within the actuator in a way that might also be coupled to feedback loops that allow autonomous, self-regulation of activity.

In the future, both the specific material and the general approach should be useful in enriching the responsive functionality of soft elastomeric materials and devices. We anticipate the development of new mechanophores that, like the materials, are reversibly and repeatedly activated, expanding the capabilities of soft, active devices and further permitting dynamic control over chemical reactivity that is otherwise inaccessible, each in response to a single remote signal.

Enhancing the numerical performance of fire field models (CMS Paper)

This paper describes two new techniques designed to enhance the performance of fire field modelling software. The two techniques are "group solvers" and automated dynamic control of the solution process, both of which are currently under development within the SMARTFIRE Computational Fluid Dynamics environment. The "group solver" is a derivation of common solver techniques used to obtain numerical solutions to the algebraic equations associated with fire field modelling. The purpose of "group solvers" is to reduce the computational overheads associated with traditional numerical solvers typically used in fire field modelling applications. In an example, discussed in this paper, the group solver is shown to provide a 37% saving in computational time compared with a traditional solver. The second technique is the automated dynamic control of the solution process, which is achieved through the use of artificial intelligence techniques. This is designed to improve the convergence capabilities of the software while further decreasing the computational overheads. The technique automatically controls solver relaxation using an integrated production rule engine with a blackboard to monitor and implement the required control changes during solution processing. Initial results for a two-dimensional fire simulation are presented that demonstrate the potential for considerable savings in simulation run-times when compared with control sets from various sources. Furthermore, the results demonstrate the potential for enhanced solution reliability due to obtaining acceptable convergence within each time step, unlike some of the comparison simulations.

Dynamic matrix control on wind-induced vibration of spatial latticed structures [Chinese title = 空间网壳结构风振抑制的动态矩阵预测控制分析]

Ameliorated strategies were put forward to improve the model predictive control in reducing the wind induced vibration of spatial latticed structures. The dynamic matrix control (DMC) predictive method was used and the reference trajectory which is called the decaying functions was suggested for the analysis of spatial latticed structure (SLS) under wind loads. The wind-induced vibration control model of SLS with improved DMC model predictive control was illustrated, then the different feedback strategies were investigated and a typical SLS was taken as example to investigate the reduction of wind-induced vibration. In addition, the robustness and reliability of DMC strategy were discussed by varying the model configurations.

Test architecture for prototyping automated dynamic airspace control

The automation of various aspects of air traffic management has many wide-reaching benefits including: reducing the workload for Air Traffic Controllers; increasing the flexibility of operations (both civil and military) within the airspace system through facilitating automated dynamic changes to en-route flight plans; ensuring safe aircraft separation for a complex mix of airspace users within a highly complex and dynamic airspace management system architecture. These benefits accumulate to increase the efficiency and flexibility of airspace use(1). Such functions are critical for the anticipated increase in volume of manned and unmanned aircraft traffic. One significant challenge facing the advancement of airspace automation lies in convincing air traffic regulatory authorities that the level of safety achievable through the use of automation concepts is comparable to, or exceeds, the accepted safety performance of the current system.

Application of Dynamic Hysteresis Band Height Control to Improve Output Voltage Transient in Boost and Positive Buck-Boost Converters

This paper presents dynamic hysteresis band height control to reduce the overshoot and undershoot issue on output voltage caused by load change. The converters in this study are Boost and Positive Buck-Boost (PBB) converters. PBB has been controlled to work in a step up conversion and avoid overshoot when load is changed. Simulation and experimental results have been presented to verify the proposed method.

Adaptive depth estimation in image based visual servo control of dynamic systems

This paper considers the question of designing a fully image based visual servo control for a dynamic system. The work is motivated by the ongoing development of image based visual servo control of small aerial robotic vehicles. The observed targets considered are coloured blobs on a flat surface to which the normal direction is known. The theoretical framework is directly applicable to the case of markings on a horizontal floor or landing field. The image features used are a first order spherical moment for position and an image flow measurement for velocity. A fully non-linear adaptive control design is provided that ensures global stability of the closed-loop system. © 2005 IEEE.