• 제목/요약/키워드: represented polynomial

검색결과 80건 처리시간 0.026초

그뢰브너 기저와 지시함수와의 관계 ($Gr\ddot{o}bner$ basis versus indicator function)

  • 김형순;박동권
    • Journal of the Korean Data and Information Science Society
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    • 제20권6호
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    • pp.1015-1027
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    • 2009
  • 대수기하학적 접근이란 실험계획에서의 공간 내의 점들 즉, 기하학적 대상인 다양체에 대한 문제를 다항식을 매개로 하여 아이디얼 즉, 대수적 문제로 전환하고자 한 것이라 할 수 있다. 지금까지의 연구는 완전요인실험으로부터 효율적인 부분요인실험을 선택하는 절차에 집중되어 왔다. 본 논문에서는 지금까지 연구 방법의 역의 과정을 추정해 보기로 한다. 한 부분요인실험이 선택되었을 때, 그 실험의 교락구조를 그뢰브너 기저를 구한 후 해석한다. 다음으로 그뢰브너 기저를 생성자로 활용하여 선택된 부분실험의 집합을 구별하기 위한 다항함수인 지시함수를 구하는 절차를 알아보기로 한다. 실제로 몇 가지 부분요인실험을 예로 택하여 그 과정을 수행하였다. 연산은 CoCoA 대수연산 소프트웨어를 이용하였다.

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면직물의 구성특성과 냉온감과의 상관성에 관한 연구( I ) -상대습도 $65\%$하에서- (A Study on the Relationship between Structural Characteristics of Cotton Fabrics and their Cool-and-Warm Felling (I) - at $65\%$ Relative Humidity-)

  • 장지혜
    • 한국의류학회지
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    • 제14권2호
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    • pp.152-163
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    • 1990
  • The purpose of this study is to experimentally analyze the relationship between structural characteristics of cotton fabrics and their cool-and-warm felling in order to develop more comfortable fabrics. Comfort in textile products has been emphasized as consumers preferred performance to fashion of clothing. Thermal comfort of clothing is a basic parameter of the comfort sensation which is usually represented by the cool-and-warm feeling felt by human skin. Cloo-and-warm feeling is perceived by the heat flux which transfers heat energy stored in an object to skin. We feel warm (cool) if the temperature of nerve extremity in skin ascends (descends). As cool-and-warm feeling determines the comfort sensation of clothing, it is important to develop new comfort fabrics. Although considerable works have been made on the body, clothing, and environment, there has been no research study on the structural characteristics of fabrics and their cool and warm feeling. Cool-and-warm feeling is closely related to the transient heat transfer property. This research study used the cotton fabrics manufactured in Korea as sample and measured $q_{max}$ value with thermal property measuring instrument (Thermo-Labo II type). $q_{max}$ values estimated by polynomial regression equation were compared with those observed in this study. This study also identified the structural parameters of cotton fabrics for a specific range of $q_{max}$ values. The findings of this study can be summarized as follows: 1) As the thickness, porosity and air permeability of cotton fabrics increase, $q_{max}$ value decreases. 2) As the fabric count and over factor of cotton fabrics increase, $q_{max}$ value also increases. 3) $q_{max}$ values have been estimated by simple and polynomial regression equations developed in this study. Regression curves which have been plotted by polynomial regression equations also provided with the range of structural parameters for a specific range of $q_{max}$ values of cotton fabrics. This study would be significant in that it has identified the structural Parameters for the cool-and-warm feeling of cotton fabric at $65\%$ relative humidity.

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퍼지추론 기반 다항식 RBF 뉴럴 네트워크의 설계 및 최적화 (The Design of Polynomial RBF Neural Network by Means of Fuzzy Inference System and Its Optimization)

  • 백진열;박병준;오성권
    • 전기학회논문지
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    • 제58권2호
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    • pp.399-406
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    • 2009
  • In this study, Polynomial Radial Basis Function Neural Network(pRBFNN) based on Fuzzy Inference System is designed and its parameters such as learning rate, momentum coefficient, and distributed weight (width of RBF) are optimized by means of Particle Swarm Optimization. The proposed model can be expressed as three functional module that consists of condition part, conclusion part, and inference part in the viewpoint of fuzzy rule formed in 'If-then'. In the condition part of pRBFNN as a fuzzy rule, input space is partitioned by defining kernel functions (RBFs). Here, the structure of kernel functions, namely, RBF is generated from HCM clustering algorithm. We use Gaussian type and Inverse multiquadratic type as a RBF. Besides these types of RBF, Conic RBF is also proposed and used as a kernel function. Also, in order to reflect the characteristic of dataset when partitioning input space, we consider the width of RBF defined by standard deviation of dataset. In the conclusion part, the connection weights of pRBFNN are represented as a polynomial which is the extended structure of the general RBF neural network with constant as a connection weights. Finally, the output of model is decided by the fuzzy inference of the inference part of pRBFNN. In order to evaluate the proposed model, nonlinear function with 2 inputs, waster water dataset and gas furnace time series dataset are used and the results of pRBFNN are compared with some previous models. Approximation as well as generalization abilities are discussed with these results.

PCA와 LDA를 결합한 데이터 전 처리와 다항식 기반 RBFNNs을 이용한 얼굴 인식 알고리즘 설계 (Design of Face Recognition algorithm Using PCA&LDA combined for Data Pre-Processing and Polynomial-based RBF Neural Networks)

  • 오성권;유성훈
    • 전기학회논문지
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    • 제61권5호
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    • pp.744-752
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    • 2012
  • In this study, the Polynomial-based Radial Basis Function Neural Networks is proposed as an one of the recognition part of overall face recognition system that consists of two parts such as the preprocessing part and recognition part. The design methodology and procedure of the proposed pRBFNNs are presented to obtain the solution to high-dimensional pattern recognition problems. In data preprocessing part, Principal Component Analysis(PCA) which is generally used in face recognition, which is useful to express some classes using reduction, since it is effective to maintain the rate of recognition and to reduce the amount of data at the same time. However, because of there of the whole face image, it can not guarantee the detection rate about the change of viewpoint and whole image. Thus, to compensate for the defects, Linear Discriminant Analysis(LDA) is used to enhance the separation of different classes. In this paper, we combine the PCA&LDA algorithm and design the optimized pRBFNNs for recognition module. The proposed pRBFNNs architecture consists of three functional modules such as the condition part, the conclusion part, and the inference part as fuzzy rules formed in 'If-then' format. In the condition part of fuzzy rules, input space is partitioned with Fuzzy C-Means clustering. In the conclusion part of rules, the connection weight of pRBFNNs is represented as two kinds of polynomials such as constant, and linear. The coefficients of connection weight identified with back-propagation using gradient descent method. The output of the pRBFNNs model is obtained by fuzzy inference method in the inference part of fuzzy rules. The essential design parameters (including learning rate, momentum coefficient and fuzzification coefficient) of the networks are optimized by means of Differential Evolution. The proposed pRBFNNs are applied to face image(ex Yale, AT&T) datasets and then demonstrated from the viewpoint of the output performance and recognition rate.

Massey-Omura 승산기를 위한 최적 정규원소 (The Optimal Normal Elements for Massey-Omura Multiplier)

  • 김창규
    • 정보보호학회논문지
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    • 제14권3호
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    • pp.41-48
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    • 2004
  • 유한체의 곱셈과 나눗셈은 오류정정부호와 암호시스템에서 중요한 산술 연산이다. 유한체 GF(2$^{m}$ )의 원소를 표현하기 위해 다양한 기저가 사용되며 차수가 m인 GF(2)상의 원시다항식으로 구성할 수 있다. 정규기저를 사용하면 곱셈이나 곱셈 역원의 연산을 쉽게 수행할 수 있다. 정규기저 표현을 이용하는 Massey-Omura 승산기는 동일한 2진함수를 사용하여 몇 번의 순회치환으로 곱셈 또는 나눗셈이 수행되며 논리함수의 곱셈항 수가 승산기의 복잡도를 결정한다. 유한체의 정규기저는 항상 존재한다. 그러나 주어진 원시다항식에 대해 최적의 정규원소를 구하는 것은 쉽지 않다. 본 논문에서는 정규기저의 생성 방법을 고찰하고, Massey-Omura 승산기를 이용한 곱셈 또는 곱셈 역원의 계산에서 연산의 복잡도를 최소화할 수 있는 정규기저를 각 원시다항식에 대해 구하여, 최적의 정규원소와 곱셈항의 개수를 제시한다.

생체형상가변 에어포일에 대한 비정상 박익이론 (Unsteady Thin Airfoil Theory of a Biomorphing Airfoil)

  • 한철희
    • 한국항공우주학회지
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    • 제34권3호
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    • pp.1-5
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    • 2006
  • 자연에 존재하는 새나 곤충들은 양력 및 추력을 발생하기 위하여 평균캠버선의 형상을 변화시킨다. 기존의 비정상 박익 이론들은 주로 강체 플랩핑 에어포일에 관하여 유도되어 왔다. 생체형상가변익의 비정상 공력특성을 파악하기 위하여 변형 가능한 에어포일에 대한 확장된 비정상 박익이론이 필요하다. 생체형상가변익의 비정상 공력특성을 계산하기 위해 Theodorsen의 접근방법을 확장하였다. 에어포일의 평균 캠버선은 다항식으로 나타내었다. 형상 가변익에 작용하는 비정상 공력특성을 순환항 및 비순환항으로 나누어 나타내었다. 본 이론은 플래핑운동을 하는 생체형상가변 에어포일의 비정상 공력해석 및 모핑날개의 공탄성 해석에 적용가능하다.

프레딕터.코렉터방법에 의한 터널다이오드 발진회로의 해석 (Analysis of a Tunnel-Diode Oscillator Circuit by Predictor-Corrector Method)

  • 이정한;차균현
    • 대한전자공학회논문지
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    • 제10권6호
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    • pp.45-55
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    • 1973
  • 본 논문은 한개의 터널다이오드로 구성된 시간에 무관한 비선형 회로를 논한다 부저항 소자로 구성된 비선형 회로의 해를 구하기 전에 비선형 소자의 정특성을 어떤 함수로 표시할 필요가 있다. 최소 자승법에 의해서 정특성을 표현하는 근사 다항식 커브를 구했다. 비선형 회로를 해석하기 위해서는 우선 그 회로에 관한 상태방정식이 설정되면 프레딕터·코렉터 방법에 의해서 해를 구할수 있다. 최종적으로, 비선형 회로의 안정도와 발진 조건을 논하기 위해서 limit cycle을 점철했다.

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DEVELOPMENT OF VEHICLE DYNAMICS MODEL FOR REAL-TIME ELECTRONIC CONTROL UNIT EVALUATION SYSTEM USING KINEMATIC AND COMPLIANCE TEST DATA

  • KIM S. S.;JUNG H. K.;SHIM J. S.;KIM C. W.
    • International Journal of Automotive Technology
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    • 제6권6호
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    • pp.599-604
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    • 2005
  • A functional suspension model is proposed as a kinematic describing function of the suspension, that represents the relative wheel displacement in polynomial form in terms of the vertical displacement of the wheel center and steering rack displacement. The relative velocity and acceleration of the wheel is represented in terms of first and second derivatives of the kinematic describing function. The system equations of motion for the full vehicle dynamic model are systematically derived by using velocity transformation method of multi-body dynamics. The comparison of test and simulation results demonstrates the validity of the proposed functional suspension modeling method. The model is computationally very efficient to achieve real-time simulation on TMS 320C6711 150 MHz DSP board of HILS (hardware-in-the-loop simulation) system for ECU (electronic control unit) evaluation of semi-active suspension.

On the Use of Finite Rotation Angles for Spacecraft Attitude Control

  • Kim, Chang Joo;Hur, Sung Wook;Ko, Joon Soo
    • International Journal of Aeronautical and Space Sciences
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    • 제18권2호
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    • pp.300-314
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    • 2017
  • This paper examines finite rotation angle (FRA) applications for spacecraft attitude control. The coordinate transformation matrix and the attitude kinematics represented by FRAs are introduced. The interpolation techniques for the angular orientations are thoroughly investigated using the FRAs and the results are compared to those using traditional methods. The paper proposes trajectory description techniques by using extremely smooth polynomial functions of time, which can describe point-to-point attitude maneuvers in a realizable and accurate manner with the help of unique FRA features. In addition, new controller design techniques using the FRAs are developed by combining the proposed interpolation techniques with a model predictive control framework. The proposed techniques are validated through their attitude control applications for an aggressive point-to-point maneuver. Conclusively, the FRAs provide much more flexibility than quaternions and Euler angles when describing kinematics, generating trajectories, and designing attitude controllers for spacecraft.

ASYMPTOTIC BEHAVIOR OF THE INVERSE OF TAILS OF HURWITZ ZETA FUNCTION

  • Lee, Ho-Hyeong;Park, Jong-Do
    • 대한수학회지
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    • 제57권6호
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    • pp.1535-1549
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    • 2020
  • This paper deals with the inverse of tails of Hurwitz zeta function. More precisely, for any positive integer s ≥ 2 and 0 ≤ a < 1, we give an algorithm for finding a simple form of fs,a(n) such that $$\lim_{n{\rightarrow}{\infty}}\{\({\sum\limits_{k=n}^{\infty}}{\frac{1}{(k+a)^s}}\)^{-1}-f_{s,a}(n)\}=0$$. We show that fs,a(n) is a polynomial in n-a of order s-1. All coefficients of fs,a(n) are represented in terms of Bernoulli numbers.