• Title/Summary/Keyword: 임무장비

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The Design and Reliability Analysis of A Mission-Critical Computer Using Extended Active Sparing Redundancy (확장 ASR 기법을 이용한 임무지향 컴퓨터의 설계 및 신뢰도 분석)

  • Shin, Jin-Beom;Kim, Sang-Ha
    • The KIPS Transactions:PartA
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    • v.16A no.4
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    • pp.235-244
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    • 2009
  • The mission-critical computer for air defense has to maintain its operation without any fault for a long mission time and is required to implement at low cost. Now the reliability of the mission critical-computer using Active Sparing Redundancy fault-tolerant technique is inferior to that of the computer using TMR technique. So in this paper are proposed Extended ASR(EASR) technique that provides higher reliability than that of the computer using TMR technique. The fault-tolerant performance of the implemented mission-critical computer is proven through reliability analysis and numbers of fault recovery test. Also, the reliability of the mission-critical computer using EASR technique is compared with those of computer using ASR and TMR techniques. EASR technique is very suitable to the mission-critical computer.

KARI Planetary Data System for Science Research Support in Korea Pathfinder Lunar Orbiter Program

  • Kim, Joo Hyeon
    • The Bulletin of The Korean Astronomical Society
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    • v.44 no.1
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    • pp.55.3-55.3
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    • 2019
  • 우리나라 최초의 우주탐사 프로그램인 Korea Pathfinder Lunar Orbiter (KPLO)는 1년의 임무기간동안 달과 달 주변의 우주환경에 대한 과학탐사 임무를 수행할 예정이다. 이를 위해서 1개에 기술 검증장비와 고해상도 카메라를 포함한 5개의 과학장비를 탑재할 예정이다. 이 중 고해상도 카메라인 LUTI(LUnar Terrain Imager)와 국내에서 개발한 3개의 과학탑재체(KGRS;감마선분광기, KMAG;자기장측정기, PolCam;광시야 편광카메라)가 획득한 과학자료는 일정기간(통상 1년)동안 비공개로 검보정이 이루어진 후 일반에게 공개(Public release)할 예정이다. 이러한 과학자료의 공개와 관리를 위해서 한국항공우주연구원은 KPLO 심우주 지상시스템 내에 과학자료의 공개 및 관리를 위한 KARI Planetary Data System(KPDS)을 개발하고 있다. KPDS는 미국 NASA의 PDS에서 개발하여 유럽, 일본 등에서 이미 행성탐사 과학자료의 표준으로 활용하고 있는 PDS4 표준을 준수하는 과학자료를 제공할 것이다. 본 발표를 통해서 KPDS의 운영개념과 과학자료 관리계획, 그리고 KPDS의 개발현황을 천문학계와 공유하여 KPLO에 의해서 획득된 과학자료가 많은 과학자들이 활용하여 높은 과학적 성과를 낼 수 있기를 기대한다.

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싱가폴 방위의 현주소와 향후 계획(2)

  • Jo, Geon-Hyeon
    • Defense and Technology
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    • no.7 s.137
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    • pp.42-57
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    • 1990
  • 1965년 싱가폴이 독립되었을때 싱가폴을 방어하기 위한 군대는 사실상 전혀없는 상태였다. 오늘날의 세계 추세와 같이 싱가폴도 자국을 보호하기 위해 급속히 군을 성장시켰다. 현재 싱가폴군은 자국의 영토를 보전할수 있는 현대화된 3군 체제를 유지하고 있다. 또한 싱가폴군은 외국 및 국내 방산업체 등을 통해 제작한 광범위한 무기체계로 장비되어 있다. 25년간 군을 운영해본 결과 싱가폴군은 그들의 임무를 충족하고 있고, 이러한 임무의 필요성과 조화되어 발전을 거듭하고 있다.

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세계의 신형 전투함 현황 (1)

  • Gang, Dong-Gyun
    • Defense and Technology
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    • no.3 s.181
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    • pp.64-79
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    • 1994
  • TYPE 23 함정의 기본적인 주 임무는 대잠전의 탐색 능력을 극대화하기 위한 매우 정숙한 함정으로 잠수함에 의해 탐지되는 것을 피하고 함정의 수중 탐지 장비가 최적의 성능을 발휘할 수 있도록 해 주는데 있다.

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A Study on Test & Evaluation Technique of RWR/CMDS for Survivability Improvement (생존성 향상을 위한 RWR/CMDS 시험평가 기술 연구)

  • Kim, Chanjo;Jang, Youngbae;Kim, Hyeongkyeong
    • Journal of Aerospace System Engineering
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    • v.10 no.4
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    • pp.84-89
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    • 2016
  • Electronic Warfare (EW) is the mission area responsible to establish and maintain a favorable position in the electromagnetic domain. Testing and Evaluation of EW devices on modern military aircraft to pursue this critical mission area require the use of a wide range of techniques and analytical methods to assure users of the readiness of EW system to meet the challenge of a combat environment. This paper is intended as an introductory text dedicated to EW systems (especially RWR, CMDS) test and evaluation techniques and will serve experienced engineers and program managers, as well as novice engineers, as a concise reference for EW systems' test and evaluation processes and testing resources.

A Study on Analysis and Improvement of Current Korean Army's Mine Detector (한국 군 운용 지뢰 탐지기 현실태 분석 및 개선 방안 연구)

  • Kim, Chi-Wook
    • The Journal of the Institute of Internet, Broadcasting and Communication
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    • v.13 no.5
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    • pp.229-233
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    • 2013
  • Mine detector of troops is different from other equipments. It is a base of a miner branch's combat, combat support and mission. But its notion is too obsucure and each troops' model and maker of it is so different and most of it is old type so there are a lot of malfunctions. Hence, I will define management of mine detector and figure out these days miner troops' mine detector situation. I will collect experts' opinions too. Through a discussion we could found improvement plan and develop it adequate for future operational environment. Proceeding all these courses and finally making it weaponize are the points of this writing.

A Study on Cockpit Voice Command System for Fighter Aircraft (전투기용 음성명령 시스템에 대한 연구)

  • Kim, Seongwoo;Seo, Mingi;Oh, Yunghwan;Kim, Bonggyu
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.41 no.12
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    • pp.1011-1017
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    • 2013
  • The human voice is the most natural means of communication. The need for speech recognition technology is increasing gradually to increase the ease of human and machine interface. The function of the avionics equipment is getting various and complicated in consequence of the growth of digital technology development, so that the load of pilots in the fighter aircraft must become increased since they don't concentrate only the attack function, but also operate the complicated avionics equipments. Accordingly, if speech recognition technology is applied to the aircraft cockpit as regards the operating the avionics equipments, pilots can spend their time and effort on the mission of fighter aircraft. In this paper, the cockpit voice command system applicable to the fighter aircraft has been developed and the function and the performance of the system verified.

Method for determining the optimal number of concurrent spare parts under available budget constraint (예산제약 하에서의 동시조달수리부속의 적정소요 산출)

  • 김영호;전치혁
    • Proceedings of the Korean Reliability Society Conference
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    • 2000.11a
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    • pp.321-328
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    • 2000
  • 본 연구는 새로운 장비체계 도입 시 초기 일정기간 동안 장비의 목표가용도 유지를 위해 필요한 동시조달수리부속(Concurrent Spare Parts)와 적정소요 산출에 관한 해법을 제시한다. 새로운 장비체계 도입 시 함께 보급되는 예비수리부속은 장비체계 운용에 중요한 역할을 한다. 따라서 장비체계가 주어진 임무를 수행하는 동시에 정상상태를 유지하기 위한 적정수준의 예비부속 확보가 필요하며 최소의 비용으로 장비의 가동률을 극대화 할 수 있도록 하여야 한다. 본 연구에서는 부품의 고장특성 및 수리능력을 고려한 고장분포함수를 바탕으로 각 부속별 중요도를 만족시키는 초기 수리부속 소요 결정모형과 해 산정기법을 제시하며 가용예산 제약에 따른 소요조정을 통해 최적의 예비부속 재고수준을 결정한다.

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A Study on Improvement about abnormal display of Multi Function Display for KUH (한국형 기동헬기 다기능시현기의 이상시현 개선에 관한 연구)

  • Kim, Young Mok;Chang, Joong Jin;Jun, Byung Kyu;Kim, Chang Young;Kim, Tae Hyun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.42 no.4
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    • pp.344-350
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    • 2014
  • Multi Function Display(MFD) of Korean Utility Helicopter(KUH) is the component of mission management/display control system and displays image information(navigation, flight, survivability, digital map, maintenance) acquired from Mission Computer(MC) while the aircraft is operated. It is an essential equipment for pilots to perform flight mission and it has functions of display scene control, data display, built in test(BIT) and brightness control. In this paper, it is analyzed the cause of abnormal display(flickering) on MFD and summarized the design changes to solve the defect. It is also described system safety analysis and suggested verification results of flight/ground test.

Mission Analysis Involving Hall Thruster for On-Orbit Servicing (궤도상 유지보수를 위한 홀추력기 임무해석)

  • Kwon, Kybeom
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.48 no.10
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    • pp.791-799
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    • 2020
  • Launched in October 2019, Northrop Grumman's MEV-1 was the world's first unmanned mission demonstrating the practical feasibility of on-orbit servicing. Although the concept of on-orbit servicing was proposed several decades ago, it has been developed to various mission concepts providing services such as orbit change, station keeping, propellant and equipment supply, upgrade, repair, on-orbit assembly and production, and space debris removal. The historical success of MEV-1 is expected to expand the market of on-orbit servicing for government agencies and commercial sectors worldwide. The on-orbit servicing essentially requires the utilization of a highly propellant efficient electric propulsion system due to the nature of the mission. In this study, the space mission analysis for a simple on-orbit mission involving Hall thruster is conducted, which is life extension mission for geostationary orbit satellites. In order to analyze the mission, design space exploration for various Hall thruster design variable combinations is performed. The values of design variables and operational parameters of Hall thruster suitable for the mission are proposed through design space analysis and optimization, and mission performance is derived. In addition, the direction of further improvement for the current on-orbit mission analysis process and space mission analysis involving Hall thruster is reviewed.