在這篇論文裡，我們主要有兩部分。首先，我們給了一類新的素有理函數，接下來，我們整理了一個有理函數分解的反例，並討論了Weierstrass p-函數的素性。 / In this thesis, our primary objective here is two parts. First, we give a new class of prime rational functions. Next, we study an example in the factorization of the rational functions and the primeness of the Weierstrass p-function.

We propose an algebraic construction of $(d+1)$-point $D$-optimal designs for $d$th degree polynomial regression with weight function $omega(x)ge 0$ on the interval $[a,b]$. Suppose that $omega'(x)/omega(x)$ is a rational function and the information of whether the optimal support contains the boundary points $a$ and $b$ is available. Then the problem of constructing $(d+1)$-point $D$-optimal designs can be transformed into a differential equation problem leading us to a certain matrix including a finite number of auxiliary unknown constants, which can be solved from a system of polynomial equations in those constants. Moreover, the $(d+1)$-point $D$-optimal interior support points are the zeros of a certain polynomial which the coefficients can be computed from a linear system. In most cases the $(d+1)$-point $D$-optimal designs are also the approximate $D$-optimal designs.

This paper is concerned with the problem of computing theapproximate D-optimal design for polynomial regression with weight function w(x)>0 on the design interval I=[m_0-a,m_0+a]. It is shown that if w'(x)/w(x) is a rational function on I and a is close to zero, then the problem of constructing D-optimal designs can be transformed into a differential equation problem leading us to a certain matrix including a finite number of auxiliary unknown constants, which can be approximated by a Taylor expansion. We provide a recursive algorithm to compute Taylor expansion of these constants. Moreover, the D-optimal interior support points are the zeros of a polynomial which has coefficients that can be computed from a linear system.

<p>This thesis surveys the issue of finding rational points on algebraic curves over finite fields. Since Goppa's construction of algebraic geometric codes, there has been great interest in finding curves with many rational points. Here we explain the main tools for finding rational points on a curve over a nite eld and provide the necessary background on ring and field theory. Four different articles are analyzed, the first of these articles gives a complete set of table showing the numbers of rational points for curves with genus up to 50. The other articles provide interesting constructions of covering curves: covers by the Hemitian curve, Kummer extensions and Artin-Schreier extensions. With these articles the great difficulty of finding explicit equations for curves with many rational points is overcome. With the method given by Arnaldo García in [6] we have been able to nd examples that can be used to define the lower bounds for the corresponding entries in the tables given in http: //wins.uva.nl/~geer, which to the time of writing this Thesis appear as "no information available". In fact, as the curves found are maximal, these entries no longer need a bound, they can be given by a unique entry, since the exact value of N_q(g) is now known.</p><p>At the end of the thesis an outline of the construction of Goppa codes is given and the NXL and XNL codes are presented.</p><p> </p>

This thesis surveys the issue of finding rational points on algebraic curves over finite fields. Since Goppa's construction of algebraic geometric codes, there has been great interest in finding curves with many rational points. Here we explain the main tools for finding rational points on a curve over a nite eld and provide the necessary background on ring and field theory. Four different articles are analyzed, the first of these articles gives a complete set of table showing the numbers of rational points for curves with genus up to 50. The other articles provide interesting constructions of covering curves: covers by the Hemitian curve, Kummer extensions and Artin-Schreier extensions. With these articles the great difficulty of finding explicit equations for curves with many rational points is overcome. With the method given by Arnaldo García in [6] we have been able to nd examples that can be used to define the lower bounds for the corresponding entries in the tables given in http: //wins.uva.nl/~geer, which to the time of writing this Thesis appear as "no information available". In fact, as the curves found are maximal, these entries no longer need a bound, they can be given by a unique entry, since the exact value of Nq(g) is now known. At the end of the thesis an outline of the construction of Goppa codes is given and the NXL and XNL codes are presented.

In this paper we investigate (d + 1)-point D-optimal designs for d-th degree polynomial regression with weight function w(x) > 0 on the interval [a, b]. Suppose that w'(x)/w(x) is a rational function and the information of whether the optimal support contains the boundary points a and b is available. Then the problem of constructing (d + 1)-point D-optimal designs can be transformed into a differential equation problem leading us to a certain matrix with k auxiliary unknown constants. We characterize the weight functions corresponding to the cases when k= 0 and k= 1. Then, we can solve (d + 1)-point D-optimal designs directly from differential equation (k = 0) or via eigenvalue problems (k = 1). The numerical results show us an interesting relationship between optimal designs and ordered eigenvalues.

No description available.

Orientador: Douglas Domingues Bueno / Resumo: Os fenômenos associados aos sistemas aeroelásticos definem uma importante classe de problemas envolvida no projeto de aeronaves. Algumas análises podem ser realizadas utilizando a formulação no domínio da frequência, porém, para alguns problemas específicos a análise no domínio do tempo mostra-se mais conveniente, especialmente para projeto de controladores e inclusão de não linearidades. Em particular, forças aerodinâmicas não estacionárias são tipicamente obtidas no domínio da frequência reduzida. Tais formulações não permitem de maneira direta, através de uma transformada inversa, obter modelos matemáticos no domínio do tempo e, portanto, é necessário o uso de um método de aproximação, como o de Roger-Abel. No entanto, uso deste método de aproximação apresenta algumas lacunas com relação ao significado físico e escolha dos parâmetros de atraso. Desta forma, o presente texto explora a influência dos estados de atraso demonstrando que é responsável pela correção da fase entre o movimento e as forças aerodinâmicas resultantes e, também, propõe uma forma de avaliação da qualidade da aproximação obtida. A partir da aproximação das cargas aerodinâmicas se obtém o modelo matemático do sistema aeroelástico, e através de simulações numéricas computacionais, tem-se a resposta do sistema aeroelástico no domínio do tempo devido à cargas de rajada $1-cosseno$. A partir da análise da resposta à rajada é possível avaliar condições em que a rajada se apresenta de maneira mais crítica para... (Resumo completo, clicar acesso eletrônico abaixo) / Abstract: The phenomena associated with the aeroelastic systems define an important class of problems involved in aircraft design. Some analyzes may be performed in the frequency domain, however, for some specific problems time domain analysis is more convenient, especially for controller design and the inclusion of nonlinearities. In particular, non-stationary aerodynamic forces are typically obtained in the reduced frequency domain. Such formulations do not allow, by means of an inverse transform, to obtain mathematical models in the time domain, and therefore it is necessary to use an approximation method, such as that of Roger-Abel. However, the use of this approximation method presents some gaps with respect to the physical meaning and choice of lag parameters. In this way, the present text explores the influence of the lag states demonstrating that it is responsible for the correction of the phase between the movement and the resulting aerodynamic forces and also proposes a method to evaluate the quality of the approximation achieved. From the approximation of the aerodynamic loads the mathematical model of the aeroelastic system is obtained, and through computational numerical simulations, has the response of the aeroelastic system in the time domain due to the 1-cosine gust load. From the analysis of the response to the gust, it is possible to evaluate conditions in which the gust is presented in a more critical way for the study system. / Mestre

Orientador: Sérgio Kurokawa / Resumo: Este trabalho apresenta uma proposta de representação de sistemas de aterramento elétrico diretamente no domínio do tempo, tendo como vantagem os benefícios da modelagem realizada no domínio da frequência, com os resultados fornecidos diretamente no domínio do tempo, sem passar por transformadas inversas (Laplace ou Fourier). Os modelos no domínio do tempo são facilmente inseridos nos softwares convencionais de análise transitória, onde as tensões e correntes são melhor compreendidas. A maior contribuição deste trabalho está no desenvolvimento de uma técnica capaz de representar o aterramento com elementos discretos e positivos de circuitos (resistores-R, capacitores-C e indutores-L). Assim, o circuito equivalente representativo do aterramento será sempre um circuito possível de ser implementado fisicamente. Nesta proposta o aterramento é inicialmente modelado no domínio da frequência, sua impedância harmônica é obtida e representada por meio de elementos discretos de circuitos (RLC) associados em série e/ou paralelo. Aterramentos constituídos por um eletrodo horizontal ou uma haste vertical foram representados por meio de aproximação usando o método dos mínimos quadrados (vector fitting), que permite obter a função racional equivalente à admitância do aterramento, a partir da qual são extraídos os ramos de circuitos e consequentemente o circuito equivalente. Apesar de ser possível representar uma infinidade de aterramentos, dependendo do comprimento e diâmetro do eletrodo/ha... (Resumo completo, clicar acesso eletrônico abaixo) / Doutor

Submitted by CLAUDINER MENDES DE SEIXAS null (claudiner2010@gmail.com) on 2017-10-21T02:06:24Z No. of bitstreams: 1 Tese_Claudiner_seixas_ac_dr_ilha.pdf: 3441885 bytes, checksum: 9e1f3e2ff82a0a8220457c535d4cea55 (MD5) / Approved for entry into archive by Luiz Galeffi (luizgaleffi@gmail.com) on 2017-10-26T14:27:13Z (GMT) No. of bitstreams: 1 seixas_cm_dr_ilha.pdf: 3441885 bytes, checksum: 9e1f3e2ff82a0a8220457c535d4cea55 (MD5) / Made available in DSpace on 2017-10-26T14:27:13Z (GMT). No. of bitstreams: 1 seixas_cm_dr_ilha.pdf: 3441885 bytes, checksum: 9e1f3e2ff82a0a8220457c535d4cea55 (MD5) Previous issue date: 2017-08-25 / Este trabalho apresenta uma proposta de representação de sistemas de aterramento elétrico diretamente no domínio do tempo, tendo como vantagem os benefícios da modelagem realizada no domínio da frequência, com os resultados fornecidos diretamente no domínio do tempo, sem passar por transformadas inversas (Laplace ou Fourier). Os modelos no domínio do tempo são facilmente inseridos nos softwares convencionais de análise transitória, onde as tensões e correntes são melhor compreendidas. A maior contribuição deste trabalho está no desenvolvimento de uma técnica capaz de representar o aterramento com elementos discretos e positivos de circuitos (resistores-R, capacitores-C e indutores-L). Assim, o circuito equivalente representativo do aterramento será sempre um circuito possível de ser implementado fisicamente. Nesta proposta o aterramento é inicialmente modelado no domínio da frequência, sua impedância harmônica é obtida e representada por meio de elementos discretos de circuitos (RLC) associados em série e/ou paralelo. Aterramentos constituídos por um eletrodo horizontal ou uma haste vertical foram representados por meio de aproximação usando o método dos mínimos quadrados (vector fitting), que permite obter a função racional equivalente à admitância do aterramento, a partir da qual são extraídos os ramos de circuitos e consequentemente o circuito equivalente. Apesar de ser possível representar uma infinidade de aterramentos, dependendo do comprimento e diâmetro do eletrodo/haste combinado com determinadas resistividade e permissividade elétricas do solo, esse método pode não garantir que todos os elementos RLC sejam positivos. Por isso foi desenvolvido uma nova técnica e testada em aplicações com configurações de aterramento mais complexas (malhas). Essa técnica fornece resultados precisos e garante que todos os elementos RLC serão positivos. Sua validação foi realizada comparando os resultados propostos com os resultados obtidos pelo modelo de linha de transmissão (no caso de eletrodo/haste) e pelo modelo eletromagnético híbrido HEM (no caso das malhas). Essa técnica permite o uso de qualquer modelo capaz de fornecer a impedância harmônica, podendo ser aplicada a configurações genéricas de aterramento, o que a torna muito versátil e atrativa. / This work presents a proposal to represent of electrical grounding systems directly in time domain, taking into account the benefits in frequency domain modelling, without employing inverse Laplace or Fourier transforms. The time domain models are easily inserted in conventional electromagnetic transient software, where voltages and currents are better understood. The main contribution of this work is the development of a technique that can represent grounding by discrete and positive circuits elements (R-resistors, C-capacitors and L-inductors). The representation of the grounding is an electric circuit, possible to be implemented physically. Grounding systems is initially modelled in the frequency domain, where its harmonic impedance is obtained and then represented by elements of circuit (RLC) made in series and/or parallel association. Grounding systems constituted by a horizontal electrode or a vertical rod were represented by means of an approximation using the method of the least squares (vector fitting). It reproduces the rational function equivalent to the admittance of the grounding, which branches of circuits are extracted, forming an equivalent circuit. Although it is possible to represent an infinity of groundings, depending on the length and diameter of the electrode / rod combined with certain electrical resistivity and permittivity of the soil, this technique may not guarantee that all RLC elements are positive. However, a new technique was developed and tested in more complex grounding systems (grids). This technique provides accurate results and ensures that all RLC elements will be positive. Its validation was performed comparing the proposed results with the results obtained by the TLM (Transmission Line Model) employed for the horizontal electrodes and vertical rods and by the HEM (Hybrid Electromagnetic Model) employed for grounding grids. This technique allows the use of any model capable of providing harmonic impedance, and can be applied to generic ground configurations, making it very attractive to electromagnetics transient analyses.