• 제목/요약/키워드: Design Development Test

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한국형 기동헬기 임무탑재장비체계 설계 및 입증 (Design and Verification of Mission Equipment Package System for Korean Utility Helicopter)

  • 김성우;이병화;유연운;이종훈;임종봉
    • 한국군사과학기술학회지
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    • 제14권3호
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    • pp.388-396
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    • 2011
  • Mission Equipment Package(MEP) system is a collection of avionic components that are integrated to perform the mission of the Korean Utility Helicopter(KUH). MEP system development is classified mission-critical embedded system but KUH MEP system developed including flight-critical data implementation. It is important to establish the good development and verification process for the successful system development. This paper describe the development and verification process in each phase for the KUH MEP system. MEP system design is verified through the qualification test, system failure test and compatibility test in System Integration Laboratory(SIL).

Development and Application of a Nutrition Education Game for Preschoolers

  • Oh, Yu-Jin;Kim, Dong-Sik
    • Journal of Community Nutrition
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    • 제8권4호
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    • pp.165-170
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    • 2006
  • This study was conducted to develop and apply a computer-based multimedia nutrition education program for preschoolers based on the Dick and Carey model of instructional design. The Dick and Carey model included 4 phases: analysis, design, development, and evaluation. The program's instructional goals, objectives, assessment instruments, content, examples, and practice questions with feedback were written in the design phase. To be familiar with the 5 food groups, 'Nutrition exploration' were programmed using Hyperstudio. 'Nutrition exploration' was designed as a five-session, interactive multimedia game, with each session taking about 5 minutes to complete. Nineteen preschoolers, aged 6, volunteered to participate formative evaluation. The effectiveness of the program was examined using a pre-post test design. Participants were recruited by personal contact at the individual preschool education center. The application was carried out during 4 weeks. The results showed that intervention participants significantly increased knowledge between pre-test and post-test. The results support using IMM (interactive multimedia) to disseminate nutrition education to the target population. This research provides the basis for continuing development of computer-based nutrition education materials.

비행제어시스템 설계 및 검증 절차 (Flight Control System Design and Verification Process)

  • 김종섭
    • 제어로봇시스템학회논문지
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    • 제14권8호
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    • pp.824-836
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    • 2008
  • Relaxed static stability(RSS) concept has been applied to improve aerodynamic performance of modern version supersonic jet fighter aircraft. Therefore, flight control systems are necessary to stabilize an unstable aircraft, and provides adequate handling qualities and achieve performance enhancements. Standard FCSDVP (Flight Control System Design and Verification Process) is provided to reduce development period of the flight control system. In addition, if this process is employed in developing flight control system, it reduces the trial and error for development and verification of flight control system. This paper addresses the flight control system design and verification process for the RSS aircraft utilizing design goal based on military specifications, linear and nonlinear system design and verification based on universal software, handling quality test based on HILS(Hardware In-the-Loop Simulator) environment, and ground and flight test results to verify aircraft dynamic flight responses.

고고도 모사용 소형시험장치 연구 (A Study of Simplified Test Rig for High Altitude Simulation)

  • 이지형;오종윤;박익수
    • 한국군사과학기술학회지
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    • 제7권4호
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    • pp.133-137
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    • 2004
  • A simplified test rig to simulate high-altitude environments was designed by analyzing the AEDC (Arnolds Engineering Development Center) report regarding simulated altitude testing. The test rig consists of a vacuum chamber, a supersonic nozzle connected to a cold-gas supplier and a diffuser. The preliminary tests were conducted to validate the AEDC design concepts. The test results showed that sub-atmospheric pressure(1.0psia) environments were realized inside the vacuum chamber and the design concepts were confirmed.

파라미터 해석을 통한 차량 성능 예측 기법 연구 (Study on the Prediction Technique of Vehicle Performance Using Parameter Analysis)

  • 김기창;김찬묵;김진택
    • 한국소음진동공학회논문집
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    • 제20권11호
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    • pp.995-1000
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    • 2010
  • With the development of the auto industry, the automobile manufacturers demand to shorten development period and reduce the cost. Compared with the traditional method, applying the virtual prototype is more economical. This paper presents a method for parameters sensitivity analysis and optimizing the performance of vehicle noise and vibration. The existing design processes were repeatedly analyzed with a focus on vehicle performance to decide the design parameters of dimension, thickness, mounting type of body and chassis systems in the vehicle development period. This paper describes the prediction technique of vehicle performance using L18 orthogonal array layout, quality deviation analysis and parameter sensitivity analysis for robust design. This paper analyzed the performance correlation equation through the frequency and sensitivity database according to a design factor change. The new concept is that the performance prediction is possible without repeated activities of test and analysis. This paper described the parameter analysis applications such as bush dynamic stiffness and bush void direction of rear suspension. Design engineer could efficiently decide the design variable using parameter analysis database in early design stage. These improvements can reduce man hour and test development period as well as to achieve stable NVH performance.

자율분산 역 제어시스템의 테스터 설계 연구 (A study on the tester design of Autonomous station control system)

  • 김영훈;홍순흠
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2008년도 춘계학술대회 논문집
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    • pp.1531-1535
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    • 2008
  • The Tester of Autonomous station control system is a system which can test the main function of Autonomous station control system through the data field. The purpose of this paper is to meet the system requirements and design a main function, menu and user interface using Use-case. The main function is a time-deadline test, a schedule broadcast test, a route control test and a version-up test, etc. The design of Autonomous station control system tester plays a primary role of the important document for the upcoming future system development of the tester.

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G7 고속전철 기술개발사업에서의 차량시스템 엔지니어링기술 및 시제차량 디자인 개발 (Development of Train System Engineering Technology and Exterior and Interior Design of Prototype Test Train in G7 Project for High Speed Railway Technology)

  • 정경렬;김경택;이병종;윤세균
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2003년도 춘계학술대회 논문집
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    • pp.533-541
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    • 2003
  • This paper shows the results of train system engineering technology and exterior and interior design of a prototype test train(HSR 350X) which was developed in R&D project titled 'Development of High Speed Railway Technology'. The prototype test train, which has two power cars, two motorized trailers and three trailers, is now being tested on high speed line.

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VDES 시험망 구축 및 서비스 솔루션 개발에 관한 상세설계 연구 (A Detailed Design Study on VDES Test Network Construction and Service Solution Development)

  • 최승현;김준태;박개명;장태훈;김푸름;정우진;송재민
    • 한국항해항만학회:학술대회논문집
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    • 한국항해항만학회 2019년도 추계학술대회
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    • pp.259-260
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    • 2019
  • 현재 한국의 Smart-Navigation Project를 통해서 VDES 시험망 구축 준비 및 시험용 서비스 솔루션 개발 과제를 수행하고 있다. 이 과제에서 VDES 통신망과 효율적인 서비스 제공을 위한 eNavigation 서비스 호스트/클라이언트 기능을 연동하는 구조를 설계한다. 제시한 구조는 VDES 해안국과 선박국, 게이트웨이, 서비스 호스트, 클라이언트 등의 개발 요소를 포함하고 있으며 이러한 VDES 시험망 장비들 간 연동을 위한 인터페이스 설계를 수행하였다. 본 논문에서 제시한 상세살계 연구는 VDES 시스템의 개발 요소인 메시지 정의, 인터페이스 설계, 메시지 운영 시나리오, 장비 설계 및 구현 방안 등을 포함한다. 우리는 설계된 인터페이스를 바탕으로 시험 장비를 제작 후, VDES 시험망을 위한 장비간 통합 및 연동 시험을 실내에서 진행할 예정이다. 그리고 실내시험을 통해 VDES 시험망을 충분히 시험한 후, 실제 해안국과 선박국에 시험망을 구축하여 실해역 시험을 2020년까지 진행하여 VDES 시험망의 적절성과 유효성을 검증할 예정이다.

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저공해 연소기 시험기술 (Test Methods on Development of Low Emission Gas Turbine Combustor)

  • 김형모;최영호;김동식;박부민
    • 항공우주기술
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    • 제6권1호
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    • pp.29-34
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    • 2007
  • On the stage of combustor development process, many aerodynamic and combustion characteristics are found out not by only ideal design concept but by only useful tests which are top confidentiality of technically advanced engine development companies, RR and GE, etc. In this study, test techniques of one of that company are analysed and described about some unique tests for test low emission combustors.

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