Sufficients conditions for analysis of extrema in the step-response of the linear control systems

This note deals whith the problem of extrema which may occur in the step-response of a stable linear system with real zeros and poles. Some simple sufficients conditions and necessary conditions are presented for analyses when zeros located between the dominant and fastest pole does not cause extrema in the step-response. These conditions require knowledge of the pole-zero configuration of the corresponding transfer-function.

Effect of a heat-treatment on the linear dimensional change of a hard chairside reline resin

Statement of problem. Little data are available regarding the effect of heat-treatments on the dimensional stability of hard chairside reline resins. Purpose. The objective of this in vitro study was to evaluate whether a heat-treatment improves the dimensional stability of the reline resin Duraliner II and to compare the linear dimensional changes of this material with the heat-polymerized acrylic resin Lucitone 550. Material and methods. The materials were mixed according to the manufacturer's instructions and packed into a stainless steel split mold (50.0 mm diameter and 0.5 mm thickness) with reference points (A, B, C, and D). Duraliner II specimens were polymerized for 12 minutes in water at 37°C and bench cooled to room temperature before being removed from the mold. Twelve specimens were made and divided into 2 groups: group 1 specimens (n=6) were left untreated, and group 2 specimens (n=6) were submitted to a heat-treatment in a water bath at 55°C for 10 minutes and then bench cooled to room temperature. The 6 Lucitone specimens (control group) were polymerized in a water bath for 9 hours at 71°C. The specimens were removed after the mold reached the room temperature. A Nikon optical comparator was used to measure the distances between the reference points (AB and CD) on the stainless steel mold (baseline readings) and on the specimens to the nearest 0.001 mm. Measurements were made after processing and after the specimens had been stored in distilled water at 37°C for 8 different periods of time. Data were subjected to analysis of variance with repeated measures, followed by Tukey's multiple comparison test (P<.05). Results. All specimens exhibited shrinkage after processing (control, -0.41%; group 1, -0.26%; and group 2, -0.51%). Group 1 specimens showed greater shrinkage (-1.23%) than the control (-0.23%) and group 2 (-0.81%) specimens after 60 days of storage in water (P<.05). Conclusion. Within the limitations of this study, a significant improvement of the long-term dimensional stability of the Duraliner II reline resin was observed when the specimens were heat-treated. However, the shrinkage remained considerably higher than the denture base resin Lucitone 550. Copyright © 2002 by The Editorial Council of The Journal of Prosthetic Dentistry.

Procedimento numérico para análise de vigas de alvenaria estrutural submetidas à flexão simples

Pós-graduação em Engenharia Civil - FEIS

Comparison between the performances of a linear isolator and an isolator with a geometrically nonlinear damper

Pós-graduação em Engenharia Mecânica - FEIS

Interpolação de dados de campo potencial através da camada equivalente

O uso da técnica da camada equivalente na interpolação de dados de campo potencial permite levar em consideração que a anomalia, gravimétrica ou magnética, a ser interpolada é uma função harmônica. Entretanto, esta técnica tem aplicação computacional restrita aos levantamentos com pequeno número de dados, uma vez que ela exige a solução de um problema de mínimos quadrados com ordem igual a este número. Para viabilizar a aplicação da técnica da camada equivalente aos levantamentos com grande número de dados, nós desenvolvemos o conceito de observações equivalentes e o método EGTG, que, respectivamente, diminui a demanda em memória do computador e otimiza as avaliações dos produtos internos inerentes à solução dos problemas de mínimos quadrados. Basicamente, o conceito de observações equivalentes consiste em selecionar algumas observações, entre todas as observações originais, tais que o ajuste por mínimos quadrados, que ajusta as observações selecionadas, ajusta automaticamente (dentro de um critério de tolerância pré-estabelecido) todas as demais que não foram escolhidas. As observações selecionadas são denominadas observações equivalentes e as restantes são denominadas observações redundantes. Isto corresponde a partir o sistema linear original em dois sistemas lineares com ordens menores. O primeiro com apenas as observações equivalentes e o segundo apenas com as observações redundantes, de tal forma que a solução de mínimos quadrados, obtida a partir do primeiro sistema linear, é também a solução do segundo sistema. Este procedimento possibilita ajustar todos os dados amostrados usando apenas as observações equivalentes (e não todas as observações originais) o que reduz a quantidade de operações e a utilização de memória pelo computador. O método EGTG consiste, primeiramente, em identificar o produto interno como sendo uma integração discreta de uma integral analítica conhecida e, em seguida, em substituir a integração discreta pela avaliação do resultado da integral analítica. Este método deve ser aplicado quando a avaliação da integral analítica exigir menor quantidade de cálculos do que a exigida para computar a avaliação da integral discreta. Para determinar as observações equivalentes, nós desenvolvemos dois algoritmos iterativos denominados DOE e DOEg. O primeiro algoritmo identifica as observações equivalentes do sistema linear como um todo, enquanto que o segundo as identifica em subsistemas disjuntos do sistema linear original. Cada iteração do algoritmo DOEg consiste de uma aplicação do algoritmo DOE em uma partição do sistema linear original. Na interpolação, o algoritmo DOE fornece uma superfície interpoladora que ajusta todos os dados permitindo a interpolação na forma global. O algoritmo DOEg, por outro lado, otimiza a interpolação na forma local uma vez que ele emprega somente as observações equivalentes, em contraste com os algoritmos existentes para a interpolação local que empregam todas as observações. Os métodos de interpolação utilizando a técnica da camada equivalente e o método da mínima curvatura foram comparados quanto às suas capacidades de recuperar os valores verdadeiros da anomalia durante o processo de interpolação. Os testes utilizaram dados sintéticos (produzidos por modelos de fontes prismáticas) a partir dos quais os valores interpolados sobre a malha regular foram obtidos. Estes valores interpolados foram comparados com os valores teóricos, calculados a partir do modelo de fontes sobre a mesma malha, permitindo avaliar a eficiência do método de interpolação em recuperar os verdadeiros valores da anomalia. Em todos os testes realizados o método da camada equivalente recuperou mais fielmente o valor verdadeiro da anomalia do que o método da mínima curvatura. Particularmente em situações de sub-amostragem, o método da mínima curvatura se mostrou incapaz de recuperar o valor verdadeiro da anomalia nos lugares em que ela apresentou curvaturas mais pronunciadas. Para dados adquiridos em níveis diferentes o método da mínima curvatura apresentou o seu pior desempenho, ao contrário do método da camada equivalente que realizou, simultaneamente, a interpolação e o nivelamento. Utilizando o algoritmo DOE foi possível aplicar a técnica da camada equivalente na interpolação (na forma global) dos 3137 dados de anomalia ar-livre de parte do levantamento marinho Equant-2 e 4941 dados de anomalia magnética de campo total de parte do levantamento aeromagnético Carauari-Norte. Os números de observações equivalentes identificados em cada caso foram, respectivamente, iguais a 294 e 299. Utilizando o algoritmo DOEg nós otimizamos a interpolação (na forma local) da totalidade dos dados de ambos os levantamentos citados. Todas as interpolações realizadas não seriam possíveis sem a aplicação do conceito de observações equivalentes. A proporção entre o tempo de CPU (rodando os programas no mesmo espaço de memória) gasto pelo método da mínima curvatura e pela camada equivalente (interpolação global) foi de 1:31. Esta razão para a interpolação local foi praticamente de 1:1.

Vibration Control Applied in a Semi-Active Suspension using Magneto Rheological Damper and Optimal Linear Control Design

In this paper we study the behavior of a semi-active suspension witch external vibrations. The mathematical model is proposed coupled to a magneto rheological (MR) damper. The goal of this work is stabilize of the external vibration that affect the comfort and durability an vehicle, to control these vibrations we propose the combination of two control strategies, the optimal linear control and the magneto rheological (MR) damper. The optimal linear control is a linear feedback control problem for nonlinear systems, under the optimal control theory viewpoint We also developed the optimal linear control design with the scope in to reducing the external vibrating of the nonlinear systems in a stable point. Here, we discuss the conditions that allow us to the linear optimal control for this kind of non-linear system.

Bifurcations Leading to Nonlinear Oscillations in a 3D Piecewise Linear Memristor Oscillator

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

A hybrid method for the solution of a sparse power system matrices on vector computers

This paper describes a methodology for solving a linear system of equations on vector computer. The methodology combines direct and inverse factors. The decomposition and implementation of the direct solution in a CRAY Y-MPZE/232, and the performance results are discussed.

Switching-off in a minimal time a fitzhugh-nagumo system

This paper deals with a system that describes an electrical circuitcomposed by a linear system coupled to a nonlinear one involving a tunneldiode in a flush-and-fill circuit. One of the most comprehensive models for thiskind of circuits was introduced by R. Fitzhugh in 1961, when taking on carebiological tasks. The equation has in its phase plane only two periodic solutions,namely, the unstable singular point S0 and the stable cycle Γ. If the system isat rest on S0, the natural flow of orbits seeks to switch-on the process by going- as time goes by - toward its steady-state, Γ. By using suitable controls it ispossible to reverse such natural tendency going in a minimal time from Γ toS0, switching-off in this way the system. To achieve this goal it is mandatorya minimal enough strength on controls. These facts will be shown by means ofconsiderations on the null control sets in the process.

Matrix-vector multiplication and triangular linear solver using GPGPU for symmetric positive definite matrices derived from elliptic equations

The modern GPUs are well suited for intensive computational tasks and massive parallel computation. Sparse matrix multiplication and linear triangular solver are the most important and heavily used kernels in scientific computation, and several challenges in developing a high performance kernel with the two modules is investigated. The main interest it to solve linear systems derived from the elliptic equations with triangular elements. The resulting linear system has a symmetric positive definite matrix. The sparse matrix is stored in the compressed sparse row (CSR) format. It is proposed a CUDA algorithm to execute the matrix vector multiplication using directly the CSR format. A dependence tree algorithm is used to determine which variables the linear triangular solver can determine in parallel. To increase the number of the parallel threads, a coloring graph algorithm is implemented to reorder the mesh numbering in a pre-processing phase. The proposed method is compared with parallel and serial available libraries. The results show that the proposed method improves the computation cost of the matrix vector multiplication. The pre-processing associated with the triangular solver needs to be executed just once in the proposed method. The conjugate gradient method was implemented and showed similar convergence rate for all the compared methods. The proposed method showed significant smaller execution time.

Algorithms for spacecraft formation flying navigation based on wireless positioning system measurements

Spacecraft formation flying navigation continues to receive a great deal of interest. The research presented in this dissertation focuses on developing methods for estimating spacecraft absolute and relative positions, assuming measurements of only relative positions using wireless sensors. The implementation of the extended Kalman filter to the spacecraft formation navigation problem results in high estimation errors and instabilities in state estimation at times. This is due tp the high nonlinearities in the system dynamic model. Several approaches are attempted in this dissertation aiming at increasing the estimation stability and improving the estimation accuracy. A differential geometric filter is implemented for spacecraft positions estimation. The differential geometric filter avoids the linearization step (which is always carried out in the extended Kalman filter) through a mathematical transformation that converts the nonlinear system into a linear system. A linear estimator is designed in the linear domain, and then transformed back to the physical domain. This approach demonstrated better estimation stability for spacecraft formation positions estimation, as detailed in this dissertation. The constrained Kalman filter is also implemented for spacecraft formation flying absolute positions estimation. The orbital motion of a spacecraft is characterized by two range extrema (perigee and apogee). At the extremum, the rate of change of a spacecraft’s range vanishes. This motion constraint can be used to improve the position estimation accuracy. The application of the constrained Kalman filter at only two points in the orbit causes filter instability. Two variables are introduced into the constrained Kalman filter to maintain the stability and improve the estimation accuracy. An extended Kalman filter is implemented as a benchmark for comparison with the constrained Kalman filter. Simulation results show that the constrained Kalman filter provides better estimation accuracy as compared with the extended Kalman filter. A Weighted Measurement Fusion Kalman Filter (WMFKF) is proposed in this dissertation. In wireless localizing sensors, a measurement error is proportional to the distance of the signal travels and sensor noise. In this proposed Weighted Measurement Fusion Kalman Filter, the signal traveling time delay is not modeled; however, each measurement is weighted based on the measured signal travel distance. The obtained estimation performance is compared to the standard Kalman filter in two scenarios. The first scenario assumes using a wireless local positioning system in a GPS denied environment. The second scenario assumes the availability of both the wireless local positioning system and GPS measurements. The simulation results show that the WMFKF has similar accuracy performance as the standard Kalman Filter (KF) in the GPS denied environment. However, the WMFKF maintains the position estimation error within its expected error boundary when the WLPS detection range limit is above 30km. In addition, the WMFKF has a better accuracy and stability performance when GPS is available. Also, the computational cost analysis shows that the WMFKF has less computational cost than the standard KF, and the WMFKF has higher ellipsoid error probable percentage than the standard Measurement Fusion method. A method to determine the relative attitudes between three spacecraft is developed. The method requires four direction measurements between the three spacecraft. The simulation results and covariance analysis show that the method’s error falls within a three sigma boundary without exhibiting any singularity issues. A study of the accuracy of the proposed method with respect to the shape of the spacecraft formation is also presented.

State Convergence Theory Applied to a Delayed Teleoperation System

State convergence is a control strategy that was proposed in the early 2000s to ensure stability and transparency in a teleoperation system under specific control gains values. This control strategy has been implemented for a linear system with or without time delay. This paper represents the first attempt at demonstrating, theoretically and experimentantally, that this control strategy can also be applied to a nonlinear teleoperation system with n degrees of freedom and delay in the communication channel. It is assumed that the human operator applies a constant force on the local manipulator during the teleoperation. In addition, the interaction between the remote manipulator and the environment is considered passive. Communication between the local and remote sites is made by means of a communication channel with variable time delay. In this article the theory of Lyapunov-Krasovskii was used to demonstrate that the local-remote teleoperation system is asymptotically stable.

Sequential and parallel synchronous alternating iterative methods

The so-called parallel multisplitting nonstationary iterative Model A was introduced by Bru, Elsner, and Neumann [Linear Algebra and its Applications 103:175-192 (1988)] for solving a nonsingular linear system Ax = b using a weak nonnegative multisplitting of the first type. In this paper new results are introduced when A is a monotone matrix using a weak nonnegative multisplitting of the second type and when A is a symmetric positive definite matrix using a P -regular multisplitting. Also, nonstationary alternating iterative methods are studied. Finally, combining Model A and alternating iterative methods, two new models of parallel multisplitting nonstationary iterations are introduced. When matrix A is monotone and the multisplittings are weak nonnegative of the first or of the second type, both models lead to convergent schemes. Also, when matrix A is symmetric positive definite and the multisplittings are P -regular, the schemes are also convergent.

Calmness of the Feasible Set Mapping for Linear Inequality Systems

In this paper we deal with parameterized linear inequality systems in the n-dimensional Euclidean space, whose coefficients depend continuosly on an index ranging in a compact Hausdorff space. The paper is developed in two different parametric settings: the one of only right-hand-side perturbations of the linear system, and that in which both sides of the system can be perturbed. Appealing to the backgrounds on the calmness property, and exploiting the specifics of the current linear structure, we derive different characterizations of the calmness of the feasible set mapping, and provide an operative expresion for the calmness modulus when confined to finite systems. In the paper, the role played by the Abadie constraint qualification in relation to calmness is clarified, and illustrated by different examples. We point out that this approach has the virtue of tackling the calmness property exclusively in terms of the system’s data.

Semi-analytical Q parameter estimate in linear and nonlinear transmission systems

We compare the Q parameter obtained from the semi-analytical model with scalar and vector models for two realistic transmission systems. First a linear system with a compensated dispersion map and second a soliton transmission system.