• Title/Summary/Keyword: 임무수행능력

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A Study on the Introduction and Application Plan of the Mobile Saturation Diving System for ROK Navy Salvage Operations (한국 해군의 해난구조작전을 위한 이동식 포화잠수체계 도입 및 활용방안에 관한 연구)

  • Yu, Ho-Hwi;Kang, Sin-Young;Lim, An
    • Journal of the Korean Society of Marine Environment & Safety
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    • v.21 no.4
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    • pp.389-396
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    • 2015
  • This study examined how to improve the Korean Navy diving system, particularly focused on using the mobile saturation diving system. This study determined the range of navy operations, and suggested requirements of mobile saturation diving system from the analysis of previous study and current Navy Diving system. Also, this study examined the use of military strategy in terms of its technical and applicable possibility for the enhancement of current system. In addition, the study analyzed both advantages/disadvantages of importing mobile saturation diving system products and domestic development. To review measures in installing and operating such system, this study included analysis on the effectiveness of individual platform. As the result, the study suggested requirements of mobile saturation diving system to be able to be operated by more than 6 divers for more than 17 days at more than 200m depth. And the study confirmed that there are beneficial to use mobile saturation diving system and current Navy saturation diving system together. However, it is low economical efficiency to change current Navy gas diving system to Saturation diving system. To review measures in installing and operating such system, this study suggested that second ATS-II should be built to be able to install mobile saturation diving system. Also, this study generated an utilization method of the system to use it for training when peacetime, and than it should be installed on other platform to use as additional salvage strength during wartime.

Design of L-Band-Phased Array Radar System for Space Situational Awareness (우주감시를 위한 L-Band 위상배열레이다 시스템 설계)

  • Lee, Jonghyun;Choi, Eun Jung;Moon, Hyun-Wook;Park, Joontae;Cho, Sungki;Park, Jang Hyun;Jo, Jung Hyun
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.29 no.3
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    • pp.214-224
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    • 2018
  • Continuous space development increases the occurrence probability of space hazards such as collapse of a satellite and collision between a satellite and space debris. In Korea, a space surveillance network with optical system has been developed; however, the radar technology for an independent space surveillance needs to be secured. Herein, an L-band phased array radar system for the detection and tracking of space objects is proposed to provide a number of services including collision avoidance and the prediction of re-entry events. With the mission analysis of space surveillance and the case analysis of foreign advanced radar systems, the radar parameters are defined and designed. The proposed radar system is able to detect a debris having a diameter of 10 cm at a maximum distance of 1,576 km. In addition, we confirmed the possibility of using the space surveillance mission for domestic satellites through the analysis of the detection area.

A Design Control System of Hybrid Underwater Glider and Performance Test (하이브리드 수중 글라이더의 제어 시스템 설계 및 성능 시험)

  • Ji, Dae-hyeong;Choi, Hyeung-sik;Kim, Joon-young;Jung, Dong-wook;Jeong, Seong-hoon
    • Journal of Advanced Navigation Technology
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    • v.21 no.1
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    • pp.21-29
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    • 2017
  • In this paper, we studied the control of the hybrid underwater glider (HUG), which has the advantage of high precision route search function and long-term mission capability. Dynamic modeling of HUG is based on numerical model of the attitude controller and buoyancy engine, thruster. We designed the control part considering the smooth control and precise sailing of HUG. A buoyancy engine capable of inhaling water is designed to control the buoyancy of HUG. And mass shifter carrying the battery was designed for controlling pitching motion of HUG. A control system for controlling the buoyancy engine and the attitude controller was constructed. In order to verify performance, we performed water tank test using manufactured HUG.

Stochastic Radar Beam Scheduling Using Simulated Annealing (Simulated Annealing을 이용한 추계적 레이더 빔 스케줄링 알고리즘)

  • Roh, Ji-Eun;Ahn, Chang-Soo;Kim, Seon-Joo;Jang, Dae-Sung;Choi, Han-Lim
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.23 no.2
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    • pp.196-206
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    • 2012
  • AESA radar is able to instantaneously and adaptively position and control the beam, and such adaptive beam pointing of AESA radar enables to remarkably improve the multi-mission capability, compared with mechanically scanned array radar. AESA radar brings a new challenges, radar resource management(RRM), which is a technique efficiently allocating finite resources, such as energy and time to each task in an optimal and intelligent way. Especially radar beam scheduling is the most critical component for the success of RRM. In this paper, we proposed stochastic radar beam scheduling algorithm using simulated annealing(SA), and evaluated the performance on the multi-function radar scenario. As a result, we showed that our proposed algorithm is superior to previous dispatching rule based scheduling algorithm from the viewpoint of beam processing latency and the number of scheduled beams, with real time capability.

The Development of Electromagnetic pulse Protection Capability in the Main System of a Tank Battalion (전차대대 주요체계의 EMP 방호능력 발전방안에 관한 연구)

  • Choi, Hokab;Han, Jaeduk;Son, Sangwoo;Kim, Sungkon
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.40 no.6
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    • pp.623-631
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    • 2020
  • An electromagnetic pulse (EMP) attack on a nuclear weapon or the airlift of an electronic bomb affects weapons systems, information devices, wired and wireless communication equipment, and power supply equipment. It can lead to confusion on the battlefield. The current standards for EMP protection when applied to the military are centered on fixed and mobile facilities and equipment. It is, however, important to study EMP protection for a single tactical unit centered on the weapon system. In this study, EMP protection standards were established for command and control, maneuvering and firepower systems vulnerable to EMPs, focusing on battle tanks with mobility, firepower, and shock force. Also, specific development plans for EMP protection capabilities are proposed, including the shielding and blocking of EMPs. Through the study, the Korean government intends to ensure a unit's command and control under an EMP attack as well as preserve the viability of a unit's personnel and guarantee the conditions for the execution of a mission.

A Survivability Model of an Intrusion Tolerance System (침입감내시스템의 생존성 모델)

  • Park, Bum-Joo;Park, Kie-Jin;Kim, Sung-Soo
    • The KIPS Transactions:PartA
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    • v.12A no.5 s.95
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    • pp.395-404
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    • 2005
  • There have been large concerns about survivability defined as the capability of a system to perform a mission-critical role, in a timely manner, in the presence of attacks, failures. In particular, One of the most important core technologies required for the design of the ITS(Intrusion Tolerance System) that performs continuously minimal essential services even when the computer system is partially compromised because of intrusions is the survivability one of In included the dependability analysis of a reliability and availability etc. quantitative dependability analysis of the In. In this Paper, we applied self-healing mechanism utilizing two factors of self-healing mechanism (fault model and system response), the core technology of autonomic computing to secure the protection power of the ITS and consisted of a state transition diagram of the ITS composed of a primary server and a backup server. We also defined the survivability, availability, and downtime cost of the ITS, and then performed studies on simulation experiments and two cases of vulnerability attack. Simulation results show that intrusion tolerance capability at the initial state is more important than coping capability at the attack state in terms of the dependability enhancement.

Attack Capability Analysis for Securing Self-Survival of Air Defense Weapons (대공방어무기의 자기생존성 확보를 위한 공격능력분석)

  • Kim, Sea Ill;Shin, Jin
    • Journal of the Korea Society for Simulation
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    • v.30 no.3
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    • pp.11-17
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    • 2021
  • The 30mm anti-aircraft gun has been developed with various types of weapon systems such as protective, protective complex, and wheel-type anti-aircraft artillery. The role of this anti-aircraft gun is an important anti-aircraft weapon in charge of air defense. Anti-aircraft weapons are tasked with defending the airspace from aircraft attacks. In particular, anti-aircraft weapons are organized in combination with mechanized units. And anti-aircraft weapons are prone to attack by enemies because they operate on the front lines of the battlefield. The enemy is expected to attack our troops by covering up or concealing as much as possible in order to increase their viability. Therefore, this study analyzed whether our 30mm anti-aircraft bullets could subdue the enemy in cover. This study analyzed the performance of 30mm anti-aircraft bullets using the M&S technique. For this study, live shooting and simulation method by M&S were used for the experiment. In this study, steel plate and plywood were used for the live shooting experiment. In addition, in the simulation process through M&S, this study used the PRODAS model, AUTODYN model, and Split-x model to analyze the trajectory, penetration, and fragmentation capability of 30mm anti-aircraft bullets. According to the experimental results, it has been proven that 30mm anti-aircraft bullets can destroy enemy armored vehicles. 30mm anti-aircraft bullets succeeded in quickly subduing enemies concealed in general buildings or forests. In this way, it was possible to minimize damage to allies in advance.

Development of Pressure Correction System for Surface Vessel to Ensure Reliability of Compartment Test Result (수상함 격실기밀시험 결과의 신뢰성 확보를 위한 압력 보정 시스템 개발)

  • Min, Il-Hong;Kim, Jun-Woo;Son, Gi-Joong
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.22 no.1
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    • pp.409-414
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    • 2021
  • Tightness performance that blocks compartments is important for surface ships to achieve superior mission performance and survivability in combat environments. To meet the above requirements, airtightness of the structural elements and the appropriate strength to specific areas are checked during a test run after ship construction. In particular, air tests of compartments adjacent to the water surface are performed. In an air test, air is injected into the compartment up to the test pressure of the test memo. The pressure drop value is checked after 10 minutes to determine if the requirements of the corresponding area are satisfied. In summer, however, when the influence of the outside temperature is large, a phenomenon in which the internal pressure increases during the air test was identified. This phenomenon reduces the reliability of the test result. Therefore, a system was designed to compensate for temperature changes in the compartments through this study. The developed system calculates the amount of pressure change caused by a temperature change in the compartment and outputs a correction value. The pressure change was calculated using the ideal gas equation, reflecting the maintenance, increase, and decrease in temperature during the test process. A comparison of the calculated pressure correction value with the database of NIST REFPROP revealed a difference of 0.126% to a maximum of 0.253%.

A Improvement Study on Safety Assurance of Main Landing Gear Failure for Rotary Wing Aircraft (회전익 항공기 안전 확보를 위한 주륜완충장치 결함 개선연구)

  • Choi, Jae Hyung;Chang, Min Wook;Lim, Hyun-Gyu;Lee, Je Suk
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.45 no.6
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    • pp.490-497
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    • 2017
  • The Main Landing Gear(MLG) of Rotary Wing Aircraft is an essential equipment in Landing System for pilot to perform a flight mission. It supports the fuselage at ground and absorbs the impact from the ground when landing, thereby, these functions sustain operational capability for pilot and crew. However, the A aircraft caused asymmetry and leakage hydraulic when it was stationed on the ground. Therefore, this paper summarizes pilot comments in operation which are classified by cause of occurrence and the troubleshooting process about each comment. It also describes design improvements which was derived from troubleshooting and suggests verification results of flight test.

A Method of Collision Avoidance for Autonomous Mobile Robot using the antenna, IR and ultrasonic (로봇의 자율 주행을 위한 더듬이, IR 및 초음파 센서를 이용한 충돌 회피 방법)

  • Shin, Seung-A;No, In-Ho;Hwang, Taehyun;Shin, Seok Hoon;Shim, Joobo;Oh, Mi Sun;Ko, Jooyoung;Shim, Jaechang
    • Journal of Korea Multimedia Society
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    • v.15 no.10
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    • pp.1236-1246
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    • 2012
  • Autonomous mobile robot has ability to move itself so it can access to danger area or narrow place, and send acquired data by sensors at the same time. In order to drive to directed place, it should progress to the destination without any collision to other robot. In this study, we built and realized the collision avoidance system for autonomous mobile robot. By using antenna, IR and ultrasonic Sensors for collision avoidance, we made it possible to sense the attached and long-distance obstacle, and can avoid. Also, we used wired and wireless network to send the data after the mission.