• 제목/요약/키워드: reliability space

검색결과 964건 처리시간 0.023초

Mapping the real-space distributions of galaxies in SDSS DR7

  • Shi, Feng
    • 천문학회보
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    • 제44권1호
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    • pp.78.1-78.1
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    • 2019
  • Using a method to correct redshift space distortion (RSD) for individual galaxies, we mapped the real space distributions of galaxies in the Sloan Digital Sky Survey (SDSS) Data Release 7(DR7). We use an ensemble of mock catalogs to demonstrate the reliability of this extension, showing that it allows for an accurate recovery of the real-space correlation functions and galaxy biases. We also demonstrate that, using an iterative method applied to intermediate scale clustering data, we can obtain an unbiased estimate of the growth rate of structure $f\sigma_8$, which is related to the clustering amplitude of matter, to an accuracy of $\sim 10\%$. Applying this method to the Sloan Digital Sky Survey (SDSS) Data Release 7 (DR7), we construct a real-space galaxy catalog spanning the redshift range $0.01 \leq z \leq 0.2$, which contains 584,473 galaxies in the North Galactic Cap (NGC). Using this data we, infer $0.376 \pm 0.038$ at a median redshift z=0.1, which is consistent with the WMAP9 cosmology at $1\sigma$ level. By combining this measurement with the real-space clustering of galaxies and with galaxy-galaxy weak lensing measurements for the same sets of galaxies, we are able to break the degeneracy between $f$, $\sigma_8$ and $b$. From the SDSS DR7 data alone, we obtain the following cosmological constraints at redshift $z=0.1$ for galaxies.

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Validation of KREAM Based on In-Situ Measurements of Aviation Radiation in Commercial Flights

  • Hwang, Junga;Kwak, Jaeyoung;Jo, Gyeongbok;Nam, Uk-won
    • Journal of Astronomy and Space Sciences
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    • 제37권4호
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    • pp.229-236
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    • 2020
  • There has been increasing necessity of more precise prediction and measurements of aviation radiation in Korea. For our air crew and passengers' radiation safety, we develop our own radiation prediction model of KREAM. In this paper, we validate the KREAM model based on comparison with Liulin observations. During early three months of this year, we perform total 25 experiments to measure aviation radiation exposure using Liulin-6K in commercial flights. We found that KREAM's result is very well consistent with Liulin observation in general. NAIRAS shows mostly higher results than Liulin observation, while CARI-6M shows generally lower results than the observations. The percent error of KREAM compared with Liulin observation is 10.95%. In contrast, the error for NAIRAS is 43.38% and 22.03% for CARI-6M. We found that the increase of the altitude might cause sudden increase in radiation exposure, especially for the polar route. As more comprehensive and complete analysis is required to validate KREAM's reliability to use for the public service, we plan to expand these radiation measurements with Liulin and Tissue Equivalent Proportional Counter (TEPC) in the near future.

터보부호를 이용한 계층적 시공간 부호기반 MIMO FTN 전송기법 연구 (A Study of MIMO FTN Scheme based on Layered Space Time Code using Turbo Code)

  • 박건웅;정지원
    • 한국정보통신학회논문지
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    • 제20권5호
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    • pp.895-901
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    • 2016
  • 차세대 무선 및 위성통신에서는 다양한 서비스와 함께 빠른 전송 효율, 높은 신뢰도 있는 통신을 요구하고 있으므로 본 논문에서는 전송률을 높이고 신뢰성을 향상시키는 방안 중 계층적 시공간 부호화 방식에 기반을 둔 MIMO와 FTN 기법이 통합된 새로운 전송 기법에 대한 복호 방법을 제안한다. MIMO 채널에서의 FTN 전송 기법의 간섭을 제거하기 위해 시공간 부호화 방식의 복호 방법을 BCJR 등화기와 터보 부호를 연접한 터보 등화 복호 모델을 제안하고, 시뮬레이션을 통해 기존의 터보 부호를 이용한 SISO 모델과 제안된 방식의 성능을 비교 분석하며 간섭량에 따른 성능을 분석하였다.

초등학교 내 학교숲 기능에 관한 교사 - 학생간 인식 비교 연구 (A Comparative Study on Teacher-Student Perception of Forest Function in Elementary School)

  • 김정호;이상훈;윤용한
    • 한국환경과학회지
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    • 제27권7호
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    • pp.519-529
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    • 2018
  • With rapid economic growth, the urban environment has created a problem of human physical and mental illness. In order to solve these problems, urban forests have emerged as a way to mitigate the environmental risks through improving the polluted environment of the city and improve the quality of life. As the urban forests have expanded, the school forests movement has also been taking an important place recently. The study focused on the performance of school forests by comparing the perceptions among teachers and students about their functions. The questionnaire was composed of 4 questions concerning human matters, 10 questions for space recognition, 4 questions for thermal environment, 2 questions for health promotion, and 20 total questions for composition of survey items. The reliability of the school forest function, number of tree planting areas and quantities, the harmony of the planting, and the satisfaction of the school forest were analyzed in the questionnaire conducted by the school members. Although it does not recognize school forests, it has a positive response to the green space that is built outdoors. It is considered that outdoor education and environmental education are sufficient in school forests and green spaces. The results showed that the outdoor green space was more satisfactory when compared with the general school. Teachers and students' preferences were similar to 'seasonal changes' and' trees of various colors and shapes'. The reliability analysis between each item shows that the coefficient for cronbach's ${\alpha}$ was .700 to .834. The purpose of this study is to identify the perception of forest function among school forest members and to utilize them as a basic data in the future.

Development of the Command and Data Handling System and Flight Software of BITSE

  • Park, Jongyeob;Baek, Ji-Hye;Jang, Bi-ho;Choi, Seonghwan;Kim, Jihun;Yang, Heesu;Kim, Jinhyun;Kim, Yeon-Han;Cho, Kyung-Suk;Swinski, Joseph-Paul A.;Nguyen, Hanson;Newmark, Jeffrey S.;Gopalswamy, Natchumuthuk
    • 천문학회보
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    • 제44권2호
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    • pp.57.4-57.4
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    • 2019
  • BITSE is a project of balloon-borne experiments for a next-generation solar coronagraph developed by a collaboration with KASI and NASA. The coronagraph is built to observe the linearly polarized brightness of solar corona with a polarization camera, a filter wheel, and an aperture door. For the observation, the coronagraph is supported by the power distribution unit (PDU), a pointing system WASP (Wallops Arc-Second Pointer), telemetry & telecommand system SIP (Support Instrument Package) which are developed at NASA's Goddard Space Flight Center, Wallops Flight Facility, and Columbia Scientific Balloon Facility. The BITSE Command and Data Handling (C&DH) system used a cost-off-the-shelf electronics to process all data sent and received by the coronagraph, including the support system operation by RS232/422, USB3, Ethernet, and digital and analog signals. The flight software is developed using the core Flight System (cFS) which is a reusable software framework and set of reusable software applications which take advantage of a rich heritage of successful space mission of NASA. The flight software can process encoding and decoding data, control the subsystems, and provide observation autonomy. We developed a python-based testing framework to improve software reliability. The flight software development is one of the crucial contributions of KASI and an important milestone for the next project which is developing a solar coronagraph to be installed at International Space Station.

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BIM기반 견적 모델링 데이터 신뢰성 향상을 위한 연구 (A Study of BIM based estimation Modeling data reliability improvement)

  • 김영진;김성아;진상윤
    • 한국건설관리학회논문집
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    • 제13권3호
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    • pp.43-55
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    • 2012
  • 최근 건설 산업에서 이슈가 되고 있는 BIM의 신뢰성을 판단하기 위한 방안으로 BIM 품질 검증 방안이 대두되고 있다. 그러나 현재 BIM 품질 검증은 부재간의 간섭체크, 공간 배치 등 3D Model을 검토하는 것에 국한되어 있으며, 구조, 설비, 견적과 같은 각 분야별 BIM기반 작업 결과물의 검증 방안은 부재한 실정이다. 특히 BIM기반 견적분야에서는 수량 산출의 근거인 산출식이 출력되지 않아 BIM기반 물량산출 결과물을 신뢰하지 못하는 현상이 발생하였다. BIM기반 견적 작업 결과물의 신뢰성을 향상시키기 위해 제조업에서 정의하고 있는 신뢰성 개념을 분석하고, 다년간 BIM기반 물량산출 수행 경험을 토대로 BIM기반 견적 또는 물량산출 작업의 신뢰성에 영향을 미치는 요인을 도출한 결과, 모델링 방법 및 BIM Tool의 특징에 따라 BIM기반 물량 데이터가 달라지는 것을 알 수 있었다. 따라서 본 연구에서는 BIM 기반 견적 모델링 시 모델링 방법에 따른 결과값의 분석과 IFC 파일 교환을 통해 데이터의 신뢰성을 높이는 올바른 모델링 방법 및 데이터 검증 방안을 제시하고자 한다.

와이블 분포를 이용한 다기능 다중상태 대기시스템의 신뢰도 분석 (Reliability Analysis of Multi-functional Multi-state Standby System Using Weibull Distribution)

  • 김지혜;정영배
    • 산업경영시스템학회지
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    • 제40권3호
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    • pp.138-147
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    • 2017
  • As the functions and structure of the system are complicated and elaborated, various types of structures are emerging to increase reliability in order to cope with a system requiring higher reliability. Among these, standby systems with standby components for each major component are mainly used in aircraft or power plants requiring high reliability. In this study, we consider a standby system with a multi-functional standby component in which one standby component simultaneously performs the functions of several major components. The structure of a parallel system with multifunctional standby components can also be seen in real aircraft hydraulic pump systems and is very efficient in terms of weight, space, and cost as compared to a basic standby system. All components of the system have complete operation, complete failure, only two states, and the system has multiple states depending on the state of the component. At this time, the multi-functional standby component is assumed to be in a non-operating standby state (Cold Standby) when the main component fails. In addition, the failure rate of each part follows the Weibull distribution which can be expressed as increasing type, constant type, and decreasing type according to the shape parameter. If the Weibull distribution is used, it can be applied to various environments in a realistic manner compared to the exponential distribution that can be reflected only when the failure rate is constant. In this paper, Markov chain analysis method is applied to evaluate the reliability of multi-functional multi-state standby system. In order to verify the validity of the reliability, a graph was generated by applying arbitrary shape parameters and scale parameter values through Excel. In order to analyze the effect of multi-functional multi-state standby system using Weibull distribution, we compared the reliability based on the most basic parallel system and the standby system.

Reliability analysis of slopes stabilised with piles using response surface method

  • Saseendran, Ramanandan;Dodagoudar, G.R.
    • Geomechanics and Engineering
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    • 제21권6호
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    • pp.513-525
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    • 2020
  • Slopes stabilised with piles are seldom analysed considering uncertainties in the parameters of the pile-slope system. Reliability analysis of the pile-slope system quantifies the degree of uncertainties and evaluates the safety of the system. In the present study, the reliability analysis of a slope stabilised with piles is performed using the first-order reliability method (FORM) based on Hasofer-Lind approach. The implicit performance function associated with the factor of safety (FS) of the slope is approximated using the response surface method. The analyses are carried out considering the design matrices formulated based on both the 2k factorial design augmented with a centre run (2k fact-centred design) and face-centered cube design (FCD). The finite element method is used as the deterministic model to compute the FS of the pile-slope system. Results are compared with the results of the Monte Carlo simulation. It is observed that the optimum location of the row of piles is at the middle of the slope to achieve the maximum FS. The results show that the reliability of the system is not uniform for different pile configurations, even if the system deterministically satisfies the target factor of safety (FSt) criterion. The FSt should be selected judiciously as it is observed that the reliability of the system changes drastically with the FSt level. The results of the 2k fact-centred design and FCD are in good agreement with each other. The procedure of the FCD is computationally costly and hence the use of 2k fact-centred design is recommended, provided the response of the system is sufficiently linear over the factorial space.

Dynamic Simulation and Analysis of the Space Shuttle Main Engine with Artificially Injected Faults

  • Cha, Jihyoung;Ha, Chulsu;Koo, Jaye;Ko, Sangho
    • International Journal of Aeronautical and Space Sciences
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    • 제17권4호
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    • pp.535-550
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    • 2016
  • Securing the safety and the reliability of liquid-propellant rocket engines (LREs) for space vehicles is indispensable as engines consist of many complex components and operate under extremely high energy-dense conditions. Thus, health monitoring has become a mandatory requirement, especially for the reusable LREs that are currently being developed. In this context, a dynamic simulation program based on MATLAB/Simulink was developed in the current research on the Space Shuttle Main Engine (SSME), a partly reusable engine. Then, a series of fault simulations using this program was conducted: at a steady state operating condition (104% Rated Propulsion Level), various simulated fault conditions were artificially injected into the simulation models for the five major valves, the pumps, and the turbines of the SSME. The consequent effects due to each fault were analyzed based on the time responses of the major parameters of the engine. It is believed that this research topic is an essential pre-step for the development of fault detection and diagnosis algorithms for reusable engines in the future.

평균속도 개념을 적용한 상태공간에서의 과도응답해석 (A Transient Response Analysis in the State-space Applying the Average Velocity Concept)

  • 김병옥;김영철;김영춘;이안성
    • 한국소음진동공학회논문집
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    • 제14권5호
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    • pp.424-431
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    • 2004
  • An implicit direct-time integration method for obtaining transient responses of general dynamic systems is described. The conventional Newmark method cannot be directly applied to state-space first-order differential equations, which contain no explicit acceleration terms. The method proposed here is the state-space Newmark method that incorporates the average velocity concept, and can be applied to an analysis of general dynamic systems that are expressed by state-space first-order differential equations. It is also readily coded into a program. Stability and accuracy analyses indicate that the method is numerically unconditionally stable like the conventional Newmark method, and has a period error of 2nd-order accuracy for small damping and 4th-order for large damping and an amplitude error of 2nd-order, regardless of damping. In addition, its utility and validity are confirmed by two application examples. The results suggest that the proposed state-space Newmark method based on average velocity be generally applied to the analysis of transient responses of general dynamic systems with a high degree of reliability with respect to stability and accuracy.