• Title/Summary/Keyword: 임무 장비

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Analysis of the Mission and Equipment Investigation by Disaster Type for the Selection of Essential Equipment for the Civil Defense Force (민방위대 필수장비 선정을 위한 재난유형별 임무 분석 및 장비 조사)

  • Park, Nam-Hee;Yeo, Hwajin
    • Proceedings of the Korean Society of Disaster Information Conference
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    • 2022.10a
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    • pp.398-399
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    • 2022
  • 민방위대 창설 이후 50여 년 동안 민방위 전반적인 분야에 많은 변화가 있었다. 민방위 분야의 주요 업무는 전시상황 및 대규모 재난상황 대비업무로 비상사태 시 국민을 보호하고, 전시 지원 업무를 수행하는 포괄적 안보 개념으로 확대된다. 그러나 1975년 민방위대 창설 50여 년간 누적된 민방위 임무 역할 변화와 복합화로 민방위 장비 운용의 효율성이 상실되고 민방위 역량을 초과하는 법적 임무 설정 등으로 현재 운영 장비의 실효성에 논란이 일고 있다. 복잡하고 다종다양한 민방위 장비 체제로는 전·평시 실제적 재난현장에서 통합 역량을 발휘하기에 제한이 있고 민방위대별 민방위 장비 보급기준이 상이하고 보급기준에 따른 임무 수행 가능 범위도 모호하여 실질적인 효과를 발휘하기도 어려운 실정이다. 본 연구는 최적·최소 임무를 기반으로 한 민방위대 편성, 교육과 장비 운용 체제를 통합 일치시킨 새로운 민방위 장비 운용체계 정립의 기초연구로써 민방위대 필수장비 선정을 위하여 재난유형별 임무를 분석하고 장비를 조사하였다.

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A Study on the System Configuration and Communication Equipment Operation for Mission and Control of Small UAV (소형 무인항공기의 임무 및 제어를 위한 시스템 구성과 통신 장비 운용에 대한 연구)

  • Ha, Young-Seok
    • Journal of Convergence for Information Technology
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    • v.9 no.11
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    • pp.118-124
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    • 2019
  • As Unmanned Aerial Vehicles technology has been widespread, various types of unmanned aircraft and mission equipment have been developed in line with mission diversification. Especially in Korea, small unmanned aerial vehicles have been actively developed. In addition, flight control system and mission equipment interface system for effective control of small unmanned aerial vehicles, efficient communication system configuration and operation for transmission to ground operated systems by processing data are required. This paper addresses efficient system structure and operation of communication equipment for missions and control of small unmanned aerial vehicles.

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

  • Song, Yong-Ha;Go, Eun-kyoung;Kwon, Sang-Eun
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.25 no.2
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    • pp.320-326
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    • 2021
  • AVTE(Air Vehicle Test Equipment) is an equipment to inspect and check the status of on-board aircraft LRUs(Line Replacement Units) before and after flight for performing successful UAV(Unmanned Aerial Vehicle) missions. This paper suggests utilization of the AVTE as an operation support-equipment by implementing several critical functions for UAV-operation on the AVTE. The AVTE easily sets initialization(default) data and compensates for the installation and position errors of the LRUs which provide critical mission data and situation image with pilots without additional individual operation support-equipment. Major fault list and situation image data could be downloaded after flight using the AVTE in the event of UAV emergency situation or unusual occurrence on duty as well. We anticipate the suggested operational approach of the AVTE could dramatically reduce the cost and man power for design and manufacture of additional operation support equipment and effectively diminish workload of the operator.

Mission Planning and Control Analysis Algorithms for the Safe Flight of an Unmanned Aerial Vehicle (무인항공기의 안전한 운항을 위한 임무계획/통제 분석 기법)

  • Ryu, Chul-Hyung;Ra, Sung-Woong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.33 no.3
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    • pp.71-77
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    • 2005
  • An unmanned aerial vehicle (UAV) is generally flied via a pre-planned flight path or real-time commands by an operator. To succeed in an assigned mission, analysis such as the line-of-sight analysis for communication between UAV and a ground data terminal should be performed. In this paper, various analysis algorithms which are performed by a ground control station in pre-flight and in-flight phases, are proposed for the safe flight of UAV. Note that the proposed algorithms can be applied to most UAV systems.

A Study on the Analysis of Mission Reliability in the Combat System through SysML (SysML설계기법을 통한 전투체계 임무신뢰도 분석연구)

  • Lee, Jeong-Wan;Jang, Joong Soon
    • Journal of the Korea Society for Simulation
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    • v.29 no.1
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    • pp.31-38
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    • 2020
  • Mission reliability is defined by the probability of accomplishing the requirements task that were targeted in product development, and in the case of combat systems, mission reliability is an important factor that will determine victory or defeat, unlike commercial equipment. The mission reliability of the existing domestic combat system was calculated by considering only the physical connections of the equipment involved in the mission performance, but as the equipment becomes increasingly sophisticated and complex, it is impossible to determine the mission relevance solely by physical connection. Thus, in this paper, improved mission reliability was calculated using SysML, the system design modeling language, by taking into account the functional connection as well as physical connection. Based on this research, we look forward that the mission reliability of the combat system that will be developed in the future will be used as a verification material.

Safety Design and Validation of Mission Equipment Package for Korean Utility Helicopter (KUH 임무탑재시스템의 안전성설계 및 검증)

  • Kim, Yoo-Kyung;Kim, Myung-Chin;Kim, Tae-Hyun;Yim, Jong-Bong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.38 no.8
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    • pp.813-822
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    • 2010
  • Integrated data processing for display of flight critical data and mission critical data was conducted without additional display instruments using glass cockpit design. Based on a pre-designed flight critical system and a mission critical system, this paper shows an optimal design of subsystem integration. The design satisfies safety requirements of flight control systems(FCS) and requires minimized modification of pre-designed systems. By conducting integration test using System Integration laboratory(SIL), it is confirmed that the introduced design approach meets the safety requirements of the MEP system.

휴대용 경찰장비의 사용성 평가에 관한 연구

  • 변승남;김철수;이동훈;이승원
    • Proceedings of the ESK Conference
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    • 1995.10a
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    • pp.164-171
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    • 1995
  • 본 연구의 목적은 설문조사기법을 통하여 경찰의 휴대용 장비의 사용실태를 조사하여 경찰의 작업부하 (work stress)를 가중시키는 장비와 설계요소를 규명하는데 있다. 또한 인간공학적 측면에서의 장비분석을 통 하여 경찰 임무 수행능력의 제고와 경찰의 사기전작에 기여할 수 있는 사용자 중심의 휴대용 장비개발의 필요성 을 제시하였다. 현대사회에 있어서 경찰은 타 직종에 비해 그 작업부하(work sterss)의 수준이 매우 높으며, 더 우기 다양한 원인에 의한 재해 가능성 또한 커서 위험한 직업으로 평가 된다. 이러한 이유로 인해 상당수의 경찰 관등이 여러 직업성 질환에 노출되고 있다. 설문조사 분석결과, 현재 사용되고 있는 휴대용 장비 중 무전기, 경찰 혁대, 경찰단화, 정모, 근무복, 우의, 신호봉 등 7가지 조사대상 장비 모두가 사용이 불편한 것으로 나타났고, 이 러한 불편함으로 인하여 사용자의 대부분이 신체적 불편함을 경험한 것으로 조사되었으며, 이외에도 발바닥, 머리, 다리 및 무릎 등의 부위가 불편한 것으로 나타났다. 또한 임무수행시 현재 사용되고 있는 휴대용장비가 기동성에 장애를 주며, 근무의욕 및 사기에도 크게 영향을 주는 것으로 나타났다.

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미래 디지털 환경에서의 병사체계(3)

  • Kim, In-U
    • Defense and Technology
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    • no.9 s.271
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    • pp.50-61
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    • 2001
  • 미래 디지털 전장 환경에서 병사는 하나의 전투체계로 인식되어야 하며 동시에 열상장비, 컴퓨터 및 통신장비 등을 통한 실시간 전투정보 센서로서의 임무 수행이 요구될 것이다. 이러한 요구에 부응하는 새로운 개념의 병사체계는 전투의 주체인 병사의 화기, 피복 및 휴대품 등을 포함한 포괄적인 체계를 말하며 병사의 타격능력, 지휘통제, 생존성, 임무지속성 및 기동성 향상을 위해 각 장비를 시스템화한 것으로 선진 각국 특히 미국과 나토를 중심으로 체계적인 개발이 이루어지고 있으며, 각 국가별로 자국의 요구에 부합하는 병사체계 개발에 노력을 경주하고 있다

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An analysis of UAV line-of-sight according to mission environment (임무 환경에 따른 무인항공기 가시선 분석)

  • Choi, Jun-Su;Hur, Chang-Wu
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.17 no.6
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    • pp.1414-1418
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    • 2013
  • In this paper, analyzed of UAVs operation altitude and range from the point of view of the data link. UAVs operation altitude is determined by the specification of the mission equipment and operational purposes. The link-of-sight analysis of data link equipment before deciding the unmanned aircraft operation altitude conditions should be considered. If GDT=0m installation then 32dBi antenna apply 15,779 meter is operation altitude. 44dBi antenna 7,927 meters. Operating altitude perspective, high-gain antenna is recommended of the long range communication.

Development of the MEP Integration Test Environment for Surion (수리온 임무탑재체계의 통합시험 환경개발)

  • Kim, Yoo-Kyung;Kim, Myung-Chin;Choi, Won-Woo;Oh, Woo-Seop
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.39 no.7
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    • pp.666-673
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    • 2011
  • To perform effective integration test of avionics equipments, the importance of a setup for integration test environment has been increasing in recently developed aircraft. Especially, the development of integration test equipment is necessary for minimizing the development period and reliability of integration test. This paper treats the model development for optimal working of integration test after analyzing the characteristics of each MEP equipments for Surion(KUH). Models, whose main role is troubleshooting of equipment and simulation for missing equipments, consists of dynamic, behavior, and ICD models depending on the dynamic characteristics. Software test for both unit level and system level are performed to verify the model reliability. By conducting integration test using SIL, it is confirmed that the developed models are suitable for integration function test of the MEP system.