• 제목/요약/키워드: Missile System

검색결과 538건 처리시간 0.046초

시스템 모델링을 위한 설계 프로세스 단계별 UML활용 방안 연구 (On System Modeling Framework for System Design Processes Using UML)

  • 장재덕;이재천
    • 시스템엔지니어링워크숍
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    • 통권6호
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    • pp.102-106
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    • 2005
  • The MBSE design method using UML has not been well exhibited throughout the overall system design processes. There has been many different modeling usages of UML for system requirements proposed by many till now. The extension of UML to system modeling must demonstrate consistent representation rule throughout the overall processes. This study proposes the method of using UML with overal consistency to implement system design processes. to validate and verify the proposed UML approaches, a case study of ATACMS Block IA missile system design was implemented and the resulting products were shown. phases of the systems engineering design process, logical solution development, and physical solution development, were demonstrated

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${\mu}$-합성법을 이용한 탐색기 주사루프의 강인 제어 (Robust Control of a Seeker Scan Loop System Using ${\mu}$-Systheis)

  • 이호평
    • 한국정밀공학회지
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    • 제16권3호통권96호
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    • pp.180-188
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    • 1999
  • ${\mu}$-synthesis is applied to design a robust controller for a seeker scan loop system which has model uncertainty and is subject to a external disturbance due to abrupt missile maneuver. The issue of modelling a real-valued parametric uncertainty of a physical seeker scan loop system is discussed. The two-degree-of-frame control structure is employed to obtain better performance. It is shown that ${\mu}$-synthesis provides a superior framework for the robust control design of a seeker scan loop system which exhibits robust performance. The proposed robust control system satisfies design requirements, and especially shows good scanning performances for conical and rosette scan patterns despite parametric uncertainty in real system model.

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The Methodology and Case of Scientific System Engineering Management Process in Defense Space Program

  • Park, Heonjun
    • 항공우주시스템공학회지
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    • 제15권4호
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    • pp.7-10
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    • 2021
  • Including 425 Program, which is Korean military surveillance and reconnaissance satellite, there were mostly civil-driven space programs in Korea. However, there are increasing numbers of military demand-driven space program in nowadays. Furthermore, it is positive effects on launch vehicle development in Korea that the termination of Korea-U.S. missile guideline. In this paper, it emphasizes the needs of system engineering(SE) management method which meets both defense system's characteristics and space's characteristics. These characteristics are such as non-fixable after the launch, the security issue in defense system. And it also introduces SE tool, methodology and its philosophy. There are several functions that data management, issue management, risk management, and technical requirement management. Also describing its implications and direction of improvement.

고기동 BTT 미사일 시스템의 통합 시뮬레이션을 위한 GUI 구현 (Design of 3D GUI Simulator for Integrated BTT Missile System)

  • 박세범;염준형;하인중
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2009년도 제40회 하계학술대회
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    • pp.1790_1791
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    • 2009
  • OpenCV을 사용하여 MFC/OpenGL 환경의 BTT 미사일을 설계하였다. 시뮬레이션을 수행 하는 동안의 이미지에서 표적의 특징점(Feature point)를 추출해 호모그래피 행렬(Homography Matrix)을 계산하여 이로부터 표적의 위치, 속도, 자세 정보등을 추정하도록 하였다. 그리고 미사일 동역학, 자동 조종 장치 역시 C로 구현하여 통합 시뮬레이션 환경을 구축하였다.

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적외선 유도무기 모의비행시험 기법 (A Hardware-In-the Loop Simulation technique for an IR guided weapon)

  • 김영주;김민희;조규필
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1993년도 한국자동제어학술회의논문집(국내학술편); Seoul National University, Seoul; 20-22 Oct. 1993
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    • pp.466-470
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    • 1993
  • A HILS(Hardware-In-the-Loop Simulation) technique for an IR guided weapon is proposed. The IR HILS facility functions as a testing unit for a missile guidance and control system to evaluate target acquisition, tracking, and countermeasure performance. The configuration of IR HILS facility, modeling technique of an IR environment including target, background and countermeasure, and test and evaluation procedure are included.

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견실한 비선형 dynamic inversion 방법을 이용한 오토파일롯 설계 (Autopilot design using robust nonlinear dynamic inversion method)

  • 김승환;송찬호
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1996년도 한국자동제어학술회의논문집(국내학술편); 포항공과대학교, 포항; 24-26 Oct. 1996
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    • pp.1492-1495
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    • 1996
  • In this paper, an approach to autopilot design based on the robust nonlinear dynamic inversion method is proposed. Both unknown parameters and uncertainty bounds are estimated and parameter estimates are used in the fast inversion. Furthermore, to get more robustness slow inversion is incorporated with MRAC(Model Reference Adaptive Control) and sliding mode control where the estimates of uncertainty bounds are used. The proposed method is applied to the pitch autopilot design of a missile system and excellent performance is shown via computer simulation.

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지능 제어 기법을 이용한 유도탄 자동 조정 장치 설계 (Design of an missile autopilot using intelligent control technique)

  • 김윤식;한웅기;국태용
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1996년도 한국자동제어학술회의논문집(국내학술편); 포항공과대학교, 포항; 24-26 Oct. 1996
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    • pp.1509-1512
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    • 1996
  • This paper presents an intelligent autopilot for STT missiles with multiple controllers. The mixed H$_{2}$/H$_{\infty}$ control technique is applied for each controller and implemented by using the genetic searching algorithm. To facilitate automatic switching of multiple controllers under different operating conditions, an error based switching scheme is also combined with the multiple controllers at the higher level, which constitutes a hierarchical intelligent control system. It is shown via computer simulation that the proposed autopilot outperforms the conventional one..

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시각화-시뮬레이션방법을 이용한 단거리미사일시스템의 성능산정모델 (Short-Range Missile system Performance Evaluation model Using GUI-Type Simulation)

  • 황흥석
    • 한국시뮬레이션학회:학술대회논문집
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    • 한국시뮬레이션학회 2000년도 춘계학술대회 논문집
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    • pp.148-152
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    • 2000
  • 본 연구는 사용자 인터페이스를 고려한 시뮬레이션 방법을 이용한 단거리 미사일시스템의 성능 평가모델의 연구이다. 주요 접근 방법으로 먼저 시스템성능산정을 위한 시뮬레이션 방법을 제시하였으며 이는 관련 Data를 수집하고 이로부터 미사일의 폭발지점을 산정하고 표적의 피해산출을 위한 방법과 종합표적살상확률을 산정하는 방법 등을 포함하였다. 다음 단계로 사용자를 위한 그래픽 사용자 인터페이스(Graphic User Interface)를 고려한 입출력과정을 시각화환경으로 구현하였다. 본 연구를 위하여 전산프로그램을 개발하고 가상 Data를 이용한 예를 들고 결과를 보였다.

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2축 김발 호밍 탐색기에서의 롤운동 보상 (Roll Compensation for Homing Seekers with 2-Axis Gimbal)

  • 황익호
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2001년도 하계학술대회 논문집 D
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    • pp.1932-1934
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    • 2001
  • In this paper, a horizontal LOS(line of sight) rate estimator for conventional sea skimming ASM(anti-ship missile) is proposed. A LOS rate dynamics model in 2 axis gimbal system and in homing geometry is derived. And a new LOS rate estimator is proposed by applying a Kalman filter theory to the LOS rate dynamics model. The proposed filter can estimate LOS rates with taking roll motions into account. Simulation results show the proposed filter produces smaller estimation errors than a conventional method.

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마이크로컴퓨터용 해양정보 시스템 (Microcomputer-Based Sea Information System)

  • 김종선;최윤철
    • 한국국방경영분석학회지
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    • 제15권2호
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    • pp.105-126
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    • 1989
  • A Geographic Information System (GIS) is a system designed to capture, store, manipulate, retrieve and display the data which are referenced to geographic location. With the progress of computer graphics technologies, GIS is now become applicable to microcomputer level. A prototype Sea Information System (SIS) applicable to microcomputer has been developed for serving informations related to naval operations in the special sea areas. This system includes GIS technologies, cartographic data captured through the tablet digitizer. which results immediate displaying on pen plotters. GIS provides users with menu-driven user interface for the retrieval of informations concerning military zones, patrol area of war ship, naval bases, radar sites and its search area, missile stations, and ships' current positions. The system is currently applicable to IBM PC/AT. Minimal hardware configuration consists 640k RAM, hard disk, and pen plotter or dot matrix printer.

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