• 제목/요약/키워드: model space

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A Space Model to Annual Rainfall in South Korea

  • Lee, Eui-Kyoo
    • Communications for Statistical Applications and Methods
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    • 제10권2호
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    • pp.445-456
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    • 2003
  • Spatial data are usually obtained at selected locations even though they are potentially available at all locations in a continuous region. Moreover the monitoring locations are clustered in some regions, sparse in other regions. One important goal of spatial data analysis is to predict unknown response values at any location throughout a region of interest. Thus, an appropriate space model should be set up and their estimates and predictions must be accompanied by measures of uncertainty. In this study we see that a space model proposed allows a best interpolation to annual rainfall data in South Korea.

Generalized Maximum Likelihood Estimation in a Multistate Stochastic Model

  • Yeo, Sung-Chil
    • 한국경영과학회지
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    • 제14권1호
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    • pp.1-15
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    • 1989
  • Multistate survival data with censoring often arise in biomedical experiments. In particular, a four-state space is used for cancer clinical trials. In a four-state space, each patient may either respond to a given treatment and then relapse or may progress without responding. In this four-state space, a model which combines the Markov and semi-Markov models is proposed. In this combined model, the generalized maximum likelihood estimators of the Markov and semi-Markov hazard functions are derived. These estimators are illustrated for the data collected in a study of treatments for advanced breast cancer.

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DESIGN AND IMPLEMENTATION OF TELEMETRY SYSTEM INTERFACE FOR KSLV-I

  • Kim Joonyun;Kim Bo-Gwan
    • 한국우주과학회:학술대회논문집(한국우주과학회보)
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    • 한국우주과학회 2004년도 한국우주과학회보 제13권2호
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    • pp.274-277
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    • 2004
  • KSLV (Korea Space Launch Vehicle)-I telemetry system will be composed of two telemetry streams: a lower stage telemetry stream and an upper stage telemetry stream. In this paper, the authors present design, implementation and test results of the upper stage telemetry interface for KSLV-I. The telemetry system currently is in the stage of the prototype model development, and its engineering model and flight model will be developed in the near future.

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Mathematics Model of Space Backside Resection Based on Condition Adjustment

  • Song, Weidong;Wang, Weixi
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2003년도 Proceedings of ACRS 2003 ISRS
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    • pp.1403-1405
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    • 2003
  • This paper focuses on the image correction under few GCPs, utilizes the collinearity equation, and builds up this mathematics model of space backside resection based on condition adjustment. Then calculates the adjusted elements of exterior orientation by iteration algorithm, and evaluates the precision. And demonstrates the high-precision, affection and wide-supplying-perspective of this model.

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상태공간 모형을 이용한 동적 예측 모형 설계 (A Design of One-Stage Dynamic Prediction Model with State Space Model)

  • 고명훈;윤상원;신용백
    • 산업경영시스템학회지
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    • 제18권34호
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    • pp.107-114
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    • 1995
  • The objective of this study is to design a one-stage dynamic prediction model with Kalman state space model. For a model verification, it is compared with EWMA(Exponentially Weighed Moving Average) model. The model designed in this research can be extended to process prevention control and quality monitoring.

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The Performance of Flight Model of the NISS onboard NEXTSat-1

  • Jeong, Woong-Seob;Moon, Bongkon;Park, Sung-Joon;Lee, Dae-Hee;Pyo, Jeonghyun;Park, Won-Kee;Kim, Il-Joong;Park, Youngsik;Ko, Kyeongyeon;Kim, Mingyu;Kim, Minjin;Ko, Jongwan;Im, Myungshin;Lee, Hyung Mok;Lee, Jeong-Eun;Shin, Goo-Hwan;Chae, Jangsoo;Matsumoto, Toshio
    • 천문학회보
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    • 제42권2호
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    • pp.58.1-58.1
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    • 2017
  • The NISS (Near-infrared Imaging Spectrometer for Star formation history) is the near-infrared spectro-photometric instrument optimized to the first Next Generation of small satellite (NEXTSat-1). The off-axis optics was developed to cover a wide field of view with 2 deg. ${\times}$ 2 deg. as well as a wide wavelength range from 0.95 to $2.5{\mu}m$. Considering the simple alignment scheme, afocal system was adapted in the optical components. The mechanical structures were tested under the space environment. We have obtained the accurate calibration data using our test facilities under the operational condition. After the final integration of flight model into the satellite, the communication with the satellite and the functional test were passed. The NISS will be launched in early 2018. During around 2-year operation, the spectro-photometric survey covering more than 100 square degree will be performed. To achieve the major scientific objectives for the study of the cosmic star formation in local and distant universe, the main observational targets will be nearby galaxies, galaxy clusters, star-forming regions and low background regions. Here, we report the final performance of the flight model of the NISS.

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공작기계 스핀들시스템에서 상태공간을 이용한 베어링 주변의 열거동에 대한 연구 (A Study on the Thermal Behavior of Bearing Surroundings using State-Space in Machine Tool Spindle System)

  • 신동수;정성종
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 1995년도 추계학술대회 논문집
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    • pp.1045-1049
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    • 1995
  • This paper proposes the state-space model of the thermal behavior of the spindle system to establish dynamic mathematical model of thermal characteristics in machine tool spindle system. the model is derived form physical law of heat transfer and thermoelasticity and represents the thermal behavior induced by uneven thermal expansions whitin a bearing. The model, which is sucessfully validated for two typical configurations of high speed spindle assembles, provides a tool for understanding the basis mechanics of induced thermal expansion as a function of initial preload, spindle speed and housing cooling conditions.

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Dynamic Modeling and Control of Flexible Space Structures

  • Chae, Jang-Soo;Park, Tae-Won
    • Journal of Mechanical Science and Technology
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    • 제17권12호
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    • pp.1912-1921
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    • 2003
  • This paper presents a global mode modeling of space structures and a control scheme from the practical point of view. Since the size of the satellite has become bigger and the accuracy of attitude control more strictly required, it is necessary to consider the structural flexibility of the spacecraft. Although it is well known that the finite element (FE) model can accurately model the flexibility of the satellite, there are associated problems : FE model has the system matrix with high order and does not provide any physical insights, and is available only after all structural features have been decided. Therefore, it is almost impossible to design attitude and orbit controller using FE model unless the structural features are in place. In order to deal with this problem, the control design scheme with the global mode (GM) model is suggested. This paper describes a flexible structure modeling and three-axis controller design process and demonstrates the adequate performance of the design with respect to the maneuverability by applying it to a large flexible spacecraft model.

성층화 열용량 모델을 이용한 VAV 시스템 급기 제어 시뮬레이션 (Simulation of Supply Air Control in a VAV System Using a Stratified Lumped Thermal Model)

  • 문정우;김서영;김원년;조형희
    • 설비공학논문집
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    • 제12권7호
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    • pp.632-641
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    • 2000
  • The present study concerns the simulation of supply-air control in a variable air volume (VAV) system. A stratified lumped thermal model (multi-zone model) is suggested to predict local thermal response of an air-conditioned space. The effects of various thermal parameters such as the cooling system capacity, the thermal mass of air-conditioned space, the time delay of thermal effect, and the building envelope heat transmission are investigated in detail. Further, the influence of control parameters, PI control factor and the sensor location on a VAV system is quantitatively delineated. The results obtained show that the previous homogeneous lumped thermal model (1-zone model) may predict a significantly different thermal response in the air-conditioned space according to the sensor location.

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서비스 공간에서의 유비쿼터스 상거래 비즈니스 모델 분석 및 사례연구 (U-Commerce in Service Space : Business Model Analysis and Case Study)

  • 이현석;이경전
    • 지능정보연구
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    • 제14권2호
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    • pp.45-61
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    • 2008
  • 기존의 유비쿼터스 상거래에 대한 연구는, 대부분이 상품을 판매하는 매장 공간을 배경으로 하는 연구인 반면, 서비스 공간에서의 유비쿼터스 상거래에 대한 연구는 드물게 이루어져왔다. 본 논문은 서비스 공간에서의 유비쿼터스상거래 사례(맥도날드의 터치오더 서비스)를 분석하고, 현실 사례의 한계를 극복하는 방법으로서, 서비스 공간에서 새로운 가치창출을 할 수 있는 유비쿼터스 상거래 비즈니스 모델인 Media Embedded Place 비즈니스 모델을 소개하였다. Media Embedded Place 비즈니스 모델은 비교적 이동성이 없는 테이블이나 게시판과 같은 사물에 태그를 부착하여 서비스를 제공하거나 상거래를 발생시키고 그 대가로 공간을 제공한 사업자가 인센티브를 취하는 비즈니스 모델을 일컫는데, 이 모델을 위한 시나리오와 애플리케이션들을 분석하고, Tag-Evaluation 모델을 이용한 수익성 분석 사례를 설명하였다.

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