• 제목/요약/키워드: asymptotic properties

검색결과 293건 처리시간 0.03초

Properties of the Variation of the Infrared Emission of OH/IR Stars III. The M Band Light Curves

  • Kwon, Young-Joo;Suh, Kyung-Won
    • Journal of Astronomy and Space Sciences
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    • 제27권4호
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    • pp.279-288
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    • 2010
  • To study properties of the pulsation in the infrared emission for long period variables, we have collected and analyzed the infrared observational data at M band for 12 OH/IR stars. We present the light curves using the data that cover about 30 years including recent observations of ISO and Spitzer. We use Marquardt-Levenberg algorithm to determine the pulsation periods and amplitudes and compare them with previous results of infrared and radio investigations. Generally, the newly determined pulsation parameters show much less errors because of the larger database. We find that the relationship between the pulsation period and amplitudes at M band is fairly well fitted with a simple linear equation in a wide period range. For OH 42.3-0.1, we find some evidences that the object could be a post-asymptotic giant branch star.

ASYMPTOTIC PROPERTIES OF THE HYPERBOLIC METRIC ON THE SPHERE WITH THREE CONICAL SINGULARITIES

  • Zhang, Tanran
    • 대한수학회보
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    • 제51권5호
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    • pp.1485-1502
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    • 2014
  • The explicit formula for the hyperbolic metric ${\lambda}_{{\alpha},{\beta},{\gamma}}(z){\mid}dz{\mid}$ on the thrice-punctured sphere $\mathbb{P}{\backslash}\{0,1,{\infty}\}$ with singularities of order 0 < ${\alpha}$, ${\beta}$ < 1, ${\gamma}{\leq}1$, ${\alpha}+{\beta}+{\gamma}$ > 2 at 0, 1, ${\infty}$ was given by Kraus, Roth and Sugawa in [9]. In this article we investigate the asymptotic properties of the higher order derivatives of ${\lambda}_{{\alpha},{\beta},{\gamma}}(z)$ near the origin and give more precise descriptions for the asymptotic behavior of ${\lambda}_{{\alpha},{\beta},{\gamma}}(z)$.

CONSISTENCY AND ASYMPTOTIC NORMALITY OF A MODIFIED LIKELIHOOD APPROACH CONTINUAL REASSESSMENT METHOD

  • Kang, Seung-Ho
    • Journal of the Korean Statistical Society
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    • 제32권1호
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    • pp.33-46
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    • 2003
  • The continual reassessment method (CRM) provides a Bayesian estimation of the maximum tolerated dose (MTD) in phase I clinical trials. The CRM has been proposed as an alternative design of the standard design. The CRM has been modified to improve practical feasibility and, recently, the likelihood approach CRM has been proposed. In this paper we investigate the consistency and asymptotic normality of the modified likelihood approach CRM in which the maximum likelihood estimate is used instead of the posterior mean. Small-sample properties of the consistency is examined using complete enumeration. Both the asymptotic results and their small-sample properties show that the modified CRML outperforms the standard design.

A Kernel-function-based Approach to Sequential Estimation with $\beta$-protection of Quantiles

  • 김성래;김성균
    • 한국전산응용수학회:학술대회논문집
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    • 한국전산응용수학회 2003년도 KSCAM 학술발표회 프로그램 및 초록집
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    • pp.14-14
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    • 2003
  • Given a sequence { $X_{n}$} of independent and identically distributed random variables with F, a sequential procedure for the p-th quantile ξ$_{P}$= $F^{-1}$ (P), 0$\beta$-protection. Some asymptotic properties for the proposed procedure and of an involved stopping time are proved: asymptotic consistency, asymptotic efficiency and asymptotic normality. From one of the results an effect of smoothing based on kernel functions is discussed. The results are also extended to the contaminated case.e.e.

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UNIFORMLY LIPSCHITZ STABILITY AND ASYMPTOTIC PROPERTY IN PERTURBED NONLINEAR DIFFERENTIAL SYSTEMS

  • CHOI, SANG IL;GOO, YOON HOE
    • 한국수학교육학회지시리즈B:순수및응용수학
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    • 제23권1호
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    • pp.1-12
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    • 2016
  • This paper shows that the solutions to the perturbed differential system $y^{\prime}=f(t, y)+\int_{to}^{t}g(s,y(s),Ty(s))ds+h(t,y(t))$ have asymptotic property and uniform Lipschitz stability. To show these properties, we impose conditions on the perturbed part $\int_{to}^{t}g(s,y(s),Ty(s))ds+h(t,y(t))$, and on the fundamental matrix of the unperturbed system y' = f(t, y).

Asymptotic 균질화법을 활용한 샌드위치패널로 제작된 위성 구조체의 동적 거동 분석 (Dynamic Behavior Analysis of a Satellite Having Sandwich Panel by Utilizing Asymptotic Homogenization)

  • 조희근
    • 한국정밀공학회지
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    • 제30권11호
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    • pp.1203-1210
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    • 2013
  • Korea's first Naro-Science small class satellite was launched by Naro launcher in 2013. The structure of the satellite is mostly composed of aluminum honeycomb and frame. The honeycomb structure is homogenized with asymptotic homogenization method and its mechanical properties were used for the numerical analysis. There have been some difficulties to modeling the honeycomb sandwich panels for FEA. In the present study, the mechanical characteristics of the sandwich panel composite were numerically computed and used for the simulation. This methodology makes it easy to overcome the weakness of modeling of complicated sandwich panels. Both an experiment of vibration test and numerical analyses were conducted simultaneously. The analysis results from the current homogenization were compared with that of experiment. It shows a good agreement on the dynamic responses and certified the reliability of the present methodology when manipulate sandwich panel structure.

Random Permutation Test for Comparison of Two Survival Curves

  • Kim, Mi-Kyung;Lee, Jae-Won;Lee, Myung-Hoe
    • Communications for Statistical Applications and Methods
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    • 제8권1호
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    • pp.137-145
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    • 2001
  • There are many situations in which the well-known tests such as log-rank test and Gehan-Wilcoxon test fail to detect the survival differences. Assuming large samples, these tests are developed asymptotically normal properties. Thus, they shall be called asymptotic tests in this paper, Several asymptotic tests sensitive to some specific types of survival differences have been recently proposed. This paper compares by simulations the test levels and the powers of the conventional asymptotic tests and their random permutation versions. Simulation studies show that the random permutation tests possess competitive powers compared to the corresponding asymptotic tests, keeping exact test levels even in the small sample case. It also provides the guidelines for choosing the valid and most powerful test under the given situation.

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INCLUSION AND EXCLUSION FOR FINITELY MANY TYPES OF PROPERTIES

  • Chae, Gab-Byoung;Cheong, Min-Seok;Kim, Sang-Mok
    • 호남수학학술지
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    • 제32권1호
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    • pp.113-129
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    • 2010
  • Inclusion and exclusion is used in many papers to count certain objects exactly or asymptotically. Also it is used to derive the Bonferroni inequalities in probabilistic area [6]. Inclusion and exclusion on finitely many types of properties is first used in R. Meyer [7] in probability form and first used in the paper of McKay, Palmer, Read and Robinson [8] as a form of counting version of inclusion and exclusion on two types of properties. In this paper, we provide a proof for inclusion and exclusion on finitely many types of properties in counting version. As an example, the asymptotic number of general cubic graphs via inclusion and exclusion formula is given for this generalization.

2-2형 압전복합체 제작 및 등가 물성 도출 (Fabrication of a 2-2 Mode Piezocomposite and Derivation of its Equivalent Properties)

  • 신호섭;노용래
    • 한국음향학회지
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    • 제30권8호
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    • pp.436-445
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    • 2011
  • 본 논문에서는 2-2형 압전복합체의 등가 물성 도출에 관해 연구하였다. 먼저 2-2 압전복합체의 특성 변화를 유한요소법으로 해석하였고, 해석 결과와 2-2 압전복합체 시제작품의 특성 측정 결과를 비교하여 유한요소해석의 타당성을 검증하였다. PZT-5H와 고분자재료로 구성된 압전복합체의 단일상 등가물성은 Asymptotic Averaging Method를 이용하여 도출하였고, 도출된 물성을 다양한 진동 모드의 단일상 공진자 유한요소 모델에 대입한 후 완전한 2-2 압전복합체와의 임피던스 스펙트럼 차이를 최소 자승법을 이용하여 보정함으로써, 도출된 등가 물성값의 정확성을 향상시켰다. 본 연구에서 도출한 2-2 압전복합체의 등가 물성은 향후 다양한 음향 센서의 설계에 유용하게 사용될 수 있을 것이다.

복합재 로터 블레이드의 구조 최적설계 (Structural Optimum Design of Composite Rotor Blade)

  • 박정진;이민우;배재성;이수용;김석우
    • 항공우주시스템공학회지
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    • 제1권3호
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    • pp.26-31
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    • 2007
  • This paper addresses a method for structural optimum design of composite rotor blade. The basic model of a composite helicopter main rotor blade is designed and its parameters determining the structural/dynamic properties are studied. Through the investigation of flap/lag/torsional stiffness, the structural properties of the model are analyzed. In this study, helicopter rotor blades are analyzed by using VABS. The computer program VABS (Variational Asymptotic Beam Section Analysis) uses the variational asymptotic method to split a three-dimensional nonlinear elasticity problem into a two dimensional cross-sectional analysis and a one-dimensional nonlinear beam problem. This is accomplished by taking advantage of certain small parameters inherent to beam-like structures. In addition, the rotational stability of the blade is estimated by the frequency diagram from FE analysis(MSC.Patran/Nastran) to understand its vibrational property. From the result, design parameters to determine and optimize the properties of the model are presented.

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