• Title/Summary/Keyword: Integrated Simulation System

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Current Status and Applications of Integrated Safety Assessment and Simulation Code System for ISA

  • Izquierdo, J.M.;Hortal, J.;Sanchez Perea, M.;Melendez, E.;Queral, C.;Rivas-Lewicky, J.
    • Nuclear Engineering and Technology
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    • v.49 no.2
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    • pp.295-305
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    • 2017
  • This paper reviews current status of the unified approach known as integrated safety assessment (ISA), as well as the associated SCAIS (simulation codes system for ISA) computer platform. These constitute a proposal, which is the result of collaborative action among the Nuclear Safety Council (CSN), University of Madrid (UPM), and NFQ Solutions S.L, aiming to allow independent regulatory verification of industry quantitative risk assessments. The content elaborates on discussions of the classical treatment of time in conventional probabilistic safety assessment (PSA) sequences and states important conclusions that can be used to avoid systematic and unacceptable underestimation of the failure exceedance frequencies. The unified ISA method meets this challenge by coupling deterministic and probabilistic mutual influences. The feasibility of the approach is illustrated with some examples of its application to a real size plant.

An Integrated Process Planning System and Finite Element Simulation for Multistage Cold Forging (유한요소해석을 통합한 다단 냉간단조 공정설계시스템)

  • 최재찬;김병민;이언호
    • Transactions of Materials Processing
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    • v.4 no.1
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    • pp.28-38
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    • 1995
  • An integrated process planning system can determine desirable operation sequences even if they have little experience in the design of multistage cold forging process. This system is composed of seven major modules such as input module, pre-design module, formability check module, forming sequence design module, forming analysis module, FEM verification module, and output module which are used independently or in all. The forming sequence for the part can be determined by means of primitive geometries such as cylinder, cone, convex, and concave. By utilizing this geometrical characteristics(diameter, height, and radius), the part geometry is expressed by a list of the primitive geometries. Accordingly, the forming sequence design is formulated as the search problem which starts with a billet geometry and finishes with a given product one. Using the developed system, the sequence drawing with all dimensions, which includes the dimensional tolerances and the proper sequence of operations for parts, is generated under the environment of AutoCAD. Several forming sequences generated by the planning system can be checked by the forming analysis module. The acceptable forming sequences can be verified further, using FE simulation.

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Study on the Integrated UAV Simulation Environment for the Evaluation of the Midair Collision Alarm System (공중충돌경보시스템 평가를 위한 통합 무인기 시뮬레이션환경 연구)

  • Mun, Seong-yeop;Kim, Ju-young;Lee, Dong-woo;Baek, Gyeong Min;Kim, Jin Sil;Na, Jongwhoa
    • Journal of Advanced Navigation Technology
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    • v.19 no.4
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    • pp.288-298
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    • 2015
  • For the commercialization of unmanned aircraft, we must validate the safety of the air/ground collision alert systems (CAS). The validation procedure of CAS requires the flight test which is not only expensive but also dangerous. To alleviate this problem, we need the simulation based validation process for the CAS. We developed an integrated UAV simulation (IUS) environment which interconnect the flight simulator, the Matlab/Simulink, and a target avionics simulation model. We developed the collision warning module of the TCAS and tested using IUS and flight encounter models. Using IUS, we can evaluate the performance and reliability of a target avionic system at the preliminary design stage of a development life cycle.

Study on Integrated-Flight Simulation Method Using CFT Imagery (탑재비행시험 영상을 적용한 통합비행 시뮬레이션 기법 연구)

  • Jeong, Dong Gil;Yun, Hyo Seok;Park, Jin Hyen
    • Journal of the Korea Society for Simulation
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    • v.27 no.1
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    • pp.111-117
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    • 2018
  • It is indispensable for a missile to track a target under the flight condition since the tracking capability affects the system performance considerably. The best way to verify the tracker's performance is flight test while it costs too much. Consequently, captive flight test or CFT has an important role in the development of a missile system. CFT, however, cannot simulate missile dynamics and is an offline and open-loop test. In this paper, we propose a new integrated-flight simulation(IFS) method using CFT imagery to overcome the limitation of synthetic image-based IFS method. This method increases the utilization of CFT's outputs and compensates the reality of imagery which lacks in the synthetic image-based IFS. Using this method make it possible to verify the system capability in various simulation modes.

Improvement of a Low Cost MEMS Inertial-GPS Integrated System Using Wavelet Denoising Techniques

  • Kang, Chang-Ho;Kim, Sun-Young;Park, Chan-Gook
    • International Journal of Aeronautical and Space Sciences
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    • v.12 no.4
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    • pp.371-378
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    • 2011
  • In this paper, the wavelet denoising techniques using thresholding method are applied to the low cost micro electromechanical system (MEMS)-global positioning system(GPS) integrated system. This was done to improve the navigation performance. The low cost MEMS signals can be distorted with conventional pre-filtering method such as low-pass filtering method. However, wavelet denoising techniques using thresholding method do not distort the rapidly-changing signals. They can reduce the signal noise. This paper verified the improvement of the navigation performance compared to the conventional pre-filtering by simulation and experiment.

The Impact of Internal heat gain on heating and Cooling Load in Curtain Wall Office Buildings (커튼월 사무소용 건물에서 실내발열이 냉난방 부하에 미치는 영향)

  • Kim, Jeong-Yoon;Yook, In-Soo;Nam, Hyun-Jin;Lee, Jin-Sung;Kim, Jae-Min;Cho, Soo
    • Proceedings of the SAREK Conference
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    • 2008.06a
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    • pp.925-930
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    • 2008
  • As office automation appliances and communication equipments are adopted in office buildings, internal heat gains increase gradually. When making simulation model, internal heat gains are usually set up with standard values or ignored. Therefore, the impact of the internal heat gains has been ignored or not been focused although it is recognised as significant contributor to heating/cooling load of buildings. This study focused on the impact of internal heat gains on curtain wall buildings. the amount and schedules of heat internal gains profiles not only affect the profiles of heating/cooling loads, but also make impact on reducing the effectiveness of high performance glazing systems. It is important to identify internal heat gains profiles before considering the installation of high performance glazing systems.

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An intelligent integrated control system for steering and traction of electric vehicles (전기자동차의 조향과 추진을 위한 지능형 통합 제어 시스템)

  • 서일홍;박명관
    • Journal of the Korean Institute of Telematics and Electronics B
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    • v.33B no.7
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    • pp.21-31
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    • 1996
  • An intelligent integrated control system is designed for the active steering and the left/right traction force distribution control of electric vehicles, where input-output linearization is employed. Also, a fuzzy-rule-based cornering force estimator is suggested to avoid using an uncertain highly nonlinear expression, and a neural network compensator is additively utilized for the estimator to correctly find cornering forece. With these techniques, the proposed control system is shown by simulation results to be robust against drastic change of the external environments such as road conditions.

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Development of the integrated management simulation system for the target correction (표적 수정이 가능한 사용자 개입 통합 관리 모의 시스템 개발)

  • Park, Woosung;Oh, TaeWon;Park, TaeHyun;Lee, YongWon;Kim, Kibum;Kwon, Kijeong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.45 no.7
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    • pp.600-609
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    • 2017
  • We designed a target management integration system that enables us to select the final target manually or automatically from seeker's sensor image. The integrated system was developed separately for the air vehicle system and the ground system. The air vehicle system simulates the motion dynamics and the sensor image of the air vehicle, and the ground system is composed of the target template image module and the ground control center module. The flight maneuver of the air vehicle is based on pseudo 6-degree of freedom motion equation and the proportional navigation guidance. The sensor image module was developed using the known infrared(IR) image rendering method, and was verified by comparing the rendered image to that of a commercial software. The ground control center module includes an user interface that can display as much information to meet user needs. Finally, we verified the integrated system with simulated impact target mission of the air vehicle, by confirming the final target change and the shot down result of the user's intervention.

A Study on the Operational Strategies of the Automated Container Terminals Using Simulation Techniques (시뮬레이션기법을 이용한 자동화 컨테이너터미널의 운용전략에 관한 연구)

  • 장성용;용운중
    • Proceedings of the Korea Society for Simulation Conference
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    • 2001.05a
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    • pp.36-42
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    • 2001
  • This paper presents the operational planning systems of automated container terminals. The proposed system is composed of berth allocation module, yard planning module, resource allocation module, sequencing module, and simulation module. All the sub-modules except resource allocation module are built into integrated simulation model using simulation package AutoMod. Simulation experiments are performed according to the number of AGVs and AGV allocation policies.

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IIR(SPKF)/FIR(MRHKF Filter) Fusion Filter and Its Performance Analysis (IIR(SPKF)/FIR(MRHKF 필터) 융합 필터 및 성능 분석)

  • Cho, Seong-Yun
    • Journal of Institute of Control, Robotics and Systems
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    • v.13 no.12
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    • pp.1230-1242
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    • 2007
  • This paper describes an IIR/FIR fusion filter for a nonlinear system, and analyzes the stability of the fusion filter. The fusion filter is applied to INS/GPS integrated system, and the performance is verified by simulation and experiment. In the fusion filter, an IIR-type filter (SPKF) and FIR-type filter (MRHKF filter) are processed independently, then the two filters are merged using the mixing probability calculated using the residuals and residual covariance information of the two filters. The merits of the SPKF and the MRHKF filter are embossed and the demerits of the filters are diminished via the filter fusion. Consequently, the proposed fusion filter has robustness against to model uncertainty, temporary disturbing noise, large initial estimation error, etc. The stability of the fusion filter is verified by showing the closeness of the states of the two sub filters in the mixing/redistribution process and the upper bound of the error covariance matrices. This fusion filter is applied into INS/GPS integrated system, and important factors for filter processing are presented. The performance of the INS/GPS integrated system designed using the fusion filter is verified by simulation under various error environments and is confirmed by experiment.