• 제목/요약/키워드: Mission Equipment

검색결과 153건 처리시간 0.027초

포병진지 구축을 위한 공병장비 최적배정 모형 (Optimum Allocation Model of Military Engineer Equipments for Artillery Position Development)

  • 장영초;이문걸
    • 경영과학
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    • 제34권2호
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    • pp.103-113
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    • 2017
  • The artillery is a key element of the ground forces operation during wartime, and the military engineers support the artillery position development operation to support the smooth operation of the artillery. In establishing the artillery position development operation plan, the commander requires more than his intuition to find the best option reflecting a number of elements of the battlefield situation which changes every minute. Moreover, the number of available equipment is smaller than the number of required position developments, and the effective equipment operation becomes essential element of this issue. This study quantified the capability of the available engineering equipment, organized a number of teams enabling equipment to put out the maximum capacity based on the quantified figures, and formed the model which allocates the team to the developing points to minimize the developing time. The goal programming method was applied to resolve the problem. The developed model was applied to compare the total mission duration following the number of teams, the variable for commander's decision, and the result of this study can be used as the quantitative data for commander's decision making process in establishing the artillery position development support operation through effective equipment management.

전투준비태세 및 유사장비 운용자료를 활용한 RAM 목표 값 설정방법에 관한 연구 (Establishing Method of RAM Objective Considering Combat Readiness and Field Data of Similarity Equipment)

  • 김경용;배석주
    • 산업경영시스템학회지
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    • 제32권3호
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    • pp.127-134
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    • 2009
  • RAM(Reliability, Availability, Maintainability) is important performance factor to keep combat readiness and optimize operational and maintenance cost of weapon systems. This paper discusses the method to establish RAM for combat readiness by using field failure data from similarity equipments. Operational availability is estimated from a binomial distribution function of user's operational conditions such as combat readiness preservation probability, operational rate, operational availability and total number of equipment. Reliability and maintainability is estimated from field failure data from similarity equipment to accomplish operational availability. The effectiveness of established RAM is verified through analysis of combat readiness preservation probability and mission reliability. A case study of weapon system illustrates the process of the proposed method.

AUV hull lines optimization with uncertainty parameters based on six sigma reliability design

  • Hou, Yuan hang;Liang, Xiao;Mu, Xu yang
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제10권4호
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    • pp.499-507
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    • 2018
  • Autonomous Underwater Vehicle (AUV), which are becoming more and more important in ocean exploitation tasks, needs energy conservation urgently when sailing the complex mission path in long time cruise. As hull lines optimization design becomes the key factor, which closely related with resistance, in AUV preliminary design stage, uncertainty parameters need to be considered seriously. In this research, Myring axial symmetry revolution body with parameterized expression is assumed as AUV hull lines, and its travelling resistance is obtained via modified DATCOM formula. The problems of AUV hull lines design for the minimum travelling resistance with uncertain parameters are studied. Based on reliability-based optimization design technology, Design For Six Sigma (DFSS) for high quality level is conducted, and is proved more reliability for the actual environment disturbance.

이중충격파형 충격시험장비를 이용한 충격시험 결과 및 분석 (The Shock-Test Result and Analysis Using Dual-Pulse Shock Testing Machine)

  • 배종수
    • 한국군사과학기술학회지
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    • 제21권3호
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    • pp.342-348
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    • 2018
  • The important issue of equipment installed in maritime weapon system is shock survivability against underwater explosion(UNDEX). If the shock survivability of equipment should not be guaranteed, the successful mission also could not be achieved. For that reason, the shock-resistance of each equipment under UNDEX environment should be demonstrated before deployment at combat field. However, the actual UNDEX test on the ocean is too expensive to conduct. Also, it has diverse dangerous factors. The main characteristic of UNDEX is a dual-pulse shock. The vertical shock test machine able to simulate dual pulse shock signal on the ground will be introduced in this paper. The dual-pulse shock signal presented in certain shock standard was achieved with this shock-test machine on the ground. The analytical procedure to set a test condition was verified by comparing simulation result with experiment result.

위성 데이터 전송용 2축 짐벌식 X-band 안테나 구동용 전장품 APD 열 해석 (Thermal Analysis of APD Electronics for Activation of a Spaceborne X-band 2-axis Antenna)

  • 하헌우;강수진;김태홍;오현웅
    • 항공우주시스템공학회지
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    • 제10권2호
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    • pp.1-6
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    • 2016
  • The thermal analysis of electronic equipment is required to predict the reliability of electronic equipment being loaded on a satellite. The transient heat transfer of electronic equipment that was developed recently has been generated using a large-scale integration circuit. If there is a transient heat transfer between EEE(Electric, Electronic and Electro mechanical) parts, it may lead to failure the satellite mission. In this study, we performed the thermal design and analysis for reliability of APD(Antenna Pointing Driver) electronics for activation of a spaceborne X-band 2-axis antenna. The EEE parts were designed using a thermal mathematical model without the thermal mitigation element. In addition, thermal analysis was performed based on the worst case for verifying the reliability of EEE parts. For the thermal analysis results, the thermal stability of electronic equipment has been demonstrated by satisfying the de-rating junction temperature.

MULTI-ORDER FRACTIONAL OPERATOR IN A TIME-DIFFERENTIAL FORMAL WITH BALANCE FUNCTION

  • Harikrishnan, S.;Ibrahim, Rabha W.;Kanagarajan, K.
    • Korean Journal of Mathematics
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    • 제27권1호
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    • pp.119-129
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    • 2019
  • Balance function is one of the joint factors to determine fall in risk theory. It helps to moderate the progression and riskiness of falls for detecting balance and fall risk factors. Nevertheless, the objective measures for balance function require expensive equipment with the assessment of any expertise. We establish the existence and uniqueness of a multi-order fractional differential equations based on ${\psi}$-Hilfer operator on time scales with balance function. This class describes the dynamic of time scales derivative. Our tool is based on the Schauder fixed point theorem. Here, sufficient conditions for Ulam-stability are given.

차량 탑재형 상·하역 장비의 설계와 딥러닝 객체 인식을 이용한 자동제어 방법 (Design of Vehicle-mounted Loading and Unloading Equipment and Autonomous Control Method using Deep Learning Object Detection)

  • 이순교;김선목;우효원;이석;이기백
    • 로봇학회논문지
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    • 제19권1호
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    • pp.79-91
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    • 2024
  • Large warehouses are building automation systems to increase efficiency. However, small warehouses, military bases, and local stores are unable to introduce automated logistics systems due to lack of space and budget, and are handling tasks manually, failing to improve efficiency. To solve this problem, this study designed small loading and unloading equipment that can be mounted on transportation vehicles. The equipment can be controlled remotely and is automatically controlled from the point where pallets loaded with cargo are visible using real-time video from an attached camera. Cargo recognition and control command generation for automatic control are achieved through a newly designed deep learning model. This model is designed to be optimized for loading and unloading equipment and mission environments based on the YOLOv3 structure. The trained model recognized 10 types of palettes with different shapes and colors with an average accuracy of 100% and estimated the state with an accuracy of 99.47%. In addition, control commands were created to insert forks into pallets without failure in 14 scenarios assuming actual loading and unloading situations.

다중임무 모듈형 무기체계 적용 차세대 설치 장치 실증 연구 (An Empirical Study on the Next Generation Installation Device for Application to Multi-Mission Modular Weapon Systems)

  • 안병준
    • 문화기술의 융합
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    • 제10권4호
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    • pp.757-761
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    • 2024
  • 현대전의 모자이크전을 수행하기 위한 다중임무 모듈형 함정의 획득 필요성이 증대되고 있고, 이 모듈형 함정에는 국내연구개발한 장비/체계 뿐만 아니라 해외 구매한 유무인복합체계를 함께 탑재해야 하는 상황이다. 다중임무 모듈형 시제함을 성공적으로 설계/건조하고 적기 전력화하기 위해서는 제한된 공간과 시간에서 유연하게 설치할 수있도록 신기술 적용을 필요로 한다. 하지만 기존의 용접(welding) 설치 방식은 안전상의 문제 때문에 설계/건조에 융통성을 제한하고 있음은 물론 결함 및 보완사항을 시정하는데 소요되는 비용과 시간이 과대하다는 문제점을 내재하고 있다. 따라서 본 연구는 이러한 측면에서 유연성을 제공할 수 있도록 선진해군에서 개발/적용된 차세대 설치 장치 현황과 한국 함정에 적용한 현장 실증 결과를 소개한다.

전기지상지원장비 및 관제시스템 통합 개발을 위한 유럽 표준안 현황 (ECSS E70 Standard for developing common EGSE and MCS)

  • 허윤구;최종연
    • 항공우주산업기술동향
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    • 제6권1호
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    • pp.56-64
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    • 2008
  • 위성체 총조립 및 시험(AIT; Assembly, Integration & Test)을 위한 전기지상지원장비(EGSE ; Electrical Ground Support Equipment)와 위성 임무 준비 및 운용을 위한 관제시스템(MCS; Mission Control System)은 동일한 시스템은 아니지만 많은 공통점과 호환 가능성을 갖고 있다. 하지만 우주 사업의 핵심 지상시스템인EGSE와 MCS는 사용 시기와 개발 조직이 달라서 오랫동안 별도로 개발 및 발전되어 왔다. 그러나 두 시스템이 기술적인 측면에서 유사한 기능과 역할을 하기 때문에 통합 또는 공통 개발에 대한 요구가 끊임없이 제기되고 있으며, 이미 세계적으로ECSS E70과 같은 관련 표준화 작업과 이를 바탕으로 실제 구현된 핵심 지상운영시스템의 개발이 최근에 기술적인 성숙을 이루고 있어 현재 거의 모든 우주 사업에서 핵심 지상운영시스템을 활용하거나 더 나아가 상용 제품을 적용하여 공통지상시스템을 개발하고 있다. EGSE와 MCS의 공통 기능에 관련된 표준화 작업은 ECSS를 통해 국제 표준(ISO, CCSDS 등)을 바탕으로 한 위성의 지상시스템에 대한 유럽 표준화 작업이 ECSS-E-70 Working Group에서 진행되고 있다. 여기서는 우주 산업에 관련된 표준화 단체인 ECSS에 대한 역사, 정책, 조직 및 문서 구조를 포함하여 ECSS에서 현재 진행되고 있는 지상시스템 및 운용 분야 관련 ECSS E70 표준화 작업의 내용 및 현황에 대해서 살펴보고자 한다.

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무인항공기 운용 지원을 위한 비행체 점검장비 활용에 관한 연구 (Study on Practical Use of Air Vehicle Test Equipment(AVTE) for UAV Operation Support)

  • 송용하;고은경;권상은
    • 한국정보통신학회논문지
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    • 제25권2호
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    • pp.320-326
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    • 2021
  • 비행체 점검장비는 기본적으로 항공기 임무수행을 위해 비행 전/후 탑재장비의 정상유무와 상태를 점검하기 위한 장비이다. 본 논문에서는 비행체 점검장비 내 무인항공기 운용 지원을 위한 기능을 식별, 설계 및 구현하고, 최초로 비행체 점검장비의 무인항공기 운용을 위한 추가적인 활용 방안을 제시한다. 제안하는 비행체 점검장비는 항공기의 임무 계획에 따라 변화하는 임무 및 영상 탑재장비의 초기설정 및 주요 정보를 통제하고, 주요 장비의 장착 및 위치보정 을 별도 지상 운용 장비 없이 수행할 수 있다. 또한 임무 간 비상상황 발생 시 착륙 후 이를 확인할 수 있는 영상 및 고장이력 역시 비행체 점검장비를 통하여 손쉽게 다운로딩 할 수 있다. 향후 타 무인기 체계 개발 시 본 논문에서 제시한 비행체 점검장비의 운용 지원 설계 방안을 적용하면 다수의 지상 운용 지원장비를 대체하여 추가적인 설계비용 및 운용 인력을 줄이고 항공기 정비사의 편의성을 획기적으로 향상 시킬 수 있을 것으로 기대한다.